command: 
 /usr/local/libexec/code_saturne/cs_solver --param s4_std_ke_1.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:                mar 16 giu 2015 10:22:24 CEST
  System:              Linux 3.19.0-21-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/20150616-1022
  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-01 (Minimum time step           )
       DTMAX  =    0.10000E+03 (Maximum time step           )
       DTREF  =    0.10000E+00 (Reference time step         )

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

 --- Frozen velocity field

       ICCVFG =              0 (1: frozen velocity field    )

 --- Per-variable properties

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

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

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

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


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

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

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


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


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

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

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


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


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


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


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

------------------------------------
 Variable              EPSILO IDIRCL
------------------------------------
 Velocity          0.1000E-07      1
 Pressure          0.1000E-07      1
 k                 0.1000E-07      1
 epsilon           0.1000E-07      1
------------------------------------

       IRESOL =            -1  (automatic solver choice     )
                IPOL*1000 + 0  (p conjuguate gradient       )
                            1  (Jacobi                      )
                IPOL*1000 + 2  (bicgstab                    )
                  avec IPOL    (preconditioning degree      )
       NITMAX =                (max number of iterations    )
       EPSILO =                (resolution precision        )
       IDIRCL = 0 ou 1         (shift diagonal if   
                                ISTAT=0 and no Dirichlet    )


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


 ** 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

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
 Finished reading:    mesh_input

 Extended neighborhood structures definition

 Extended neighborhood structures definition

 Extended neighborhood structures definition
 Finished reading:    mesh_input

 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

 ----------------------------------------------------------
 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:

 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


   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:

 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


   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:

 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


   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 (2.58 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+00  0.1000E+00
 ---------------------------------



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

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



==                                                             

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


 ** 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+00  0.1000E+00
 ---------------------------------



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

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



===                                                             

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


 ** 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+00  0.1000E+00
 ---------------------------------



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

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



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



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


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




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


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


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.8800E+03  0.8800E+03
  molecular_viscos  0.3960E-01  0.3960E-01
  turbulent_viscos  0.5389E+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     143   0.14141E+00   0.36867E+02 0.75431E+02 
c  Velocity[X]                                      0.18278E+01 
c  Velocity[Y]                                      0.37778E+01 
c  Velocity[Z]                                      0.31262E+02 
c  Pressure     0.38169E-01    2216   0.57437E+01   0.97860E+00 0.83895E+02 
c  k            0.52744E-02    142v  Local Time Step            0.01        0.032669        0.010068        0.012887


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier              10      3.4553e+07          3170.2          40.189


 TIME FOR THE TIME STEP                1:        0.27230E+03

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


 INSTANT    0.200000000E+00   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         0.442491694E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
----------------------------------v  Local Time Step            0.01        0.032669        0.010068        0.012887


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier              10      3.4553e+07          3170.2          40.189


 TIME FOR THE TIME STEP                1:        0.28067E+03

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


 INSTANT    0.200000000E+00   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         0.442491694E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12158E+01 0.15777E+01
   Friction velocity        uet   :  0.18240E-01 0.22872E+02
   Friction velocity        uk    :  0.17967E-01 0.22872E+02
   Dimensionless distance   yplus :  0.28055E-02 0.69344E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         84
   Nb of faces within the viscous sub-layer     :      34731
   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     0.29972E+00     921   0.14512E+00   0.10747E+02 0.32759E+02 
c  Velocity[X]                                      0.44106E+00 
c  Velocity[Y]                                      0.10191E+01 
c  Velocity[Z]                                      0.92868E+01 
c  Pressure     0.17089E+00    2001   0.10364E+01   0.34862E+01 0.22209E+02 
c  k            0.12229E-01     707   0.34686E-01   0.94955E-01 0.97651E+02 
c  epsilon      0.38384E+03     715   0.25261E-01   0.11016E+09 0.10000E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon        
a  Local Time Step      4.2277e-08                        281562


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.47583          3.0361         0.16438        0.054503
v  Velocity[Y]             -2.4899          4.7286         0.20056         0.12774
v  Velocity[Z]             -4.6463          3.3339       -0.021215        0.013387
v  ǁVelocityǁ           0.00056077          6.1261         0.50523         0.94733
v  Pressure                 25.904           17083          9393.8            8801
v  k                    1.8524e-09           2.394        0.011096        0.012137
v  epsilon              5.4335e-05      1.1233e+05          174.64           92.72
v  TurbVisc             1.1611e-12         0.47059        0.068347         0.12562
v  CourantNb              0.026613           34957          35.931          8.8093
v  FourierNb               0.27908      2.3654e+06          252.16          9.7106
v  total_pressure       5.0003e+05      5.1708e+05      5.0939e+05       5.088e+05
v  Local Time Step            0.01        0.014246        0.010001        0.010005


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

      Rel velocity at the wall uiptn : -0.13310E+01 0.18517E+01
   Friction velocity        uet   :  0.10088E-01 0.14391E+02
   Friction velocity        uk    :  0.10025E-01 0.14391E+02
   Dimensionless distance   yplus :  0.16775E-02 0.82352E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        389
   Nb of faces within the viscous sub-layer     :      34633
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.32093E+00     557   0.84728E-01   0.11992E+01 0.10361E+02 
c  Velocity[X]                                      0.22518E+00 
c  Velocity[Y]                                      0.40315E+00 
c  Velocity[Z]                                      0.57088E+00 
c  Pressure     0.69637E-01    2061   0.13424E+01   0.10385E+01 0.97872E+02 
c  k            0.99575E-02     259   0.31387E-01   0.86409E-01 0.36974E+03 
c  epsilon      0.24759E+03      87   0.36856E-01   0.10894E+09 0.65370E+04 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.004119                         15407
a  epsilon                 -107.37                          3882
a  Local Time Step      4.2278e-08                        281172


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.51842          2.7382         0.17469        0.054952
v  Velocity[Y]             -1.9739           3.574         0.19855         0.13337
v  Velocity[Z]              -3.586          3.1606       -0.033073       0.0083496
v  ǁVelocityǁ           0.00082043          5.0257         0.53368          1.0022
v  Pressure                 3.5301          8078.8          5086.2          4281.2
v  k                    8.3874e-12         0.28133      0.00066052       0.0035504
v  epsilon              2.1699e-07          5983.2          1.6893          1.2188
v  TurbVisc             3.8536e-16         0.19391         0.00386       0.0046097
v  CourantNb             0.0081703           22386          29.708          9.0284
v  FourierNb                0.2196      2.3653e+06          220.03          2.9755
v  total_pressure            5e+05      5.0808e+05      5.0509e+05      5.0428e+05
v  Local Time Step            0.01         0.01567        0.010003         0.01001


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.94564      2.3772e+06          249.74          12.004


 TIME FOR THE TIME STEP                3:        0.24909E+03

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


 INSTANT    0.400000000E+00   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         0.926223052E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet                Rel velocity at the wall uiptn : -0.13310E+01 0.18517E+01
   Friction velocity        uet   :  0.10088E-01 0.14391E+02
   Friction velocity        uk    :  0.10025E-01 0.14391E+02
   Dimensionless distance   yplus :  0.16775E-02 0.82352E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        389
   Nb of faces within the viscous sub-layer     :      34633
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.32093E+00     557   0.84728E-01   0.11992E+01 0.10361E+02 
c  Velocity[X]                                      0.22518E+00 
c  Velocity[Y]                                      0.40315E+00 
c  Velocity[Z]                                      0.57088E+00 
c  Pressure     0.69637E-01    2061   0.13424E+01   0.10385E+01 0.97872E+02 
c  k            0.99575E-02     259   0.31387E-01   0.86409E-01 0.36974E+03 
c  epsilon      0.24759E+03      87   0.36856E-01   0.10894E+09 0.65370E+04 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.004119                         15407
a  epsilon                 -107.37                          3882
a  Local Time Step      4.2278e-08                        281172


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.51842          2.7382         0.17469        0.054952
v  Velocity[Y]             -1.9739           3.574         0.19855         0.13337
v  Velocity[Z]              -3.586          3.1606       -0.033073       0.0083496
v  ǁVelocityǁ           0.00082043          5.0257         0.53368          1.0022
v  Pressure                 3.5301          8078.8          5086.2          4281.2
v  k                    8.3874e-12         0.28133      0.00066052       0.0035504
v  epsilon              2.1699e-07          5983.2          1.6893          1.2188
v  TurbVisc             3.8536e-16         0.19391         0.00386       0.0046097
v  CourantNb             0.0081703           22386          29.708          9.0284
v  FourierNb                0.2196      2.3653e+06          220.03          2.9755
v  total_pressure            5e+05      5.0808e+05      5.0509e+05      5.0428e+05
v  Local Time Step            0.01         0.01567        0.010003         0.01001


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.94564      2.3772e+06          249.74          12.004


 TIME FOR THE TIME STEP                3:        0.25514E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                      Courant/Fourier         0.97471      2.3734e+06          249.43          12.121


 TIME FOR THE TIME STEP                4:        0.24842E+03

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


 INSTANT    0.500000000E+00   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         0.127086199E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491752E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50707E+00 0.16555E+01
   Friction velocity        uet   :  0.12234E-01 0.21389E+02
   Friction velocity        uk    :  0.12203E-01 0.21389E+02
   Dimensionless distance   yplus :  0.26072E-02 0.76723E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        513
   Nb of faces within the viscous sub-layer     :      34852
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24622E+00     502   0.97764E-01   0.76711E+00 0.87954E+01 
c  Velocity[X]                                      0.13084E+00 
c  Velocity[Y]                                      0.28028E+00 
c  Velocity[Z]                                      0.35598E+00 
c  Pressure     0.79437E-01    1407   0.38896E+00   0.78398E+00 0.28248E+01 
c  k            0.79607E-02     282   0.15251E-02   0.17080E-03 0.15430E+02 
c  epsilon      0.13488E+03     101   0.99292E-03   0.10586E+05 0.57314E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.0848e-05                          4587
a  epsilon               -0.096962                          8472
a  Local Time Step      4.2278e-08                        280606


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.71871          2.5899         0.17843        0.050537
v  Velocity[Y]             -1.8959          2.9514         0.16574         0.11846
v  Velocity[Z]             -3.3293          2.7537        -0.05392      -0.0036401
v  ǁVelocityǁ           0.00034137          4.1173         0.54211           0.938
v  Pressure                -1143.3          4582.1          2989.1          2222.2
v  k                    2.3277e-15         0.42403      0.00090628       0.0039514
v  epsilon              3.5269e-12          9434.5            1.54          1.1765
v  TurbVisc     Courant/Fourier         0.97471      2.3734e+06          249.43          12.121


 TIME FOR THE TIME STEP                4:        0.24755E+03

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


 INSTANT    0.500000000E+00   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         0.127086199E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491752E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50707E+00 0.16555E+01
   Friction velocity        uet   :  0.12234E-01 0.21389E+02
   Friction velocity        uk    :  0.12203E-01 0.21389E+02
   Dimensionless distance   yplus :  0.26072E-02 0.76723E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        513
   Nb of faces within the viscous sub-layer     :      34852
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24622E+00     502   0.97764E-01   0.76711E+00 0.87954E+01 
c  Velocity[X]                                      0.13084E+00 
c  Velocity[Y]                                      0.28028E+00 
c  Velocity[Z]                                      0.35598E+00 
c  Pressure     0.79437E-01    1407   0.38896E+00   0.78398E+00 0.28248E+01 
c  k            0.79607E-02     282   0.15251E-02   0.17080E-03 0.15430E+02 
c  epsilon      0.13488E+03     101   0.99292E-03   0.10586E+05 0.57314E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.0848e-05                          4587
a  epsilon               -0.096962                          8472
a  Local Time Step      4.2278e-08                        280606


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.71871          2.5899         0.17843        0.050537
v  Velocity[Y]             -1.8959          2.9514         0.16574         0.11846
v  Velocity[Z]             -3.3293          2.7537        -0.05392      -0.0036401
v  ǁVelocityǁ           0.00034137          4.1173         0.54211           0.938
v  a  Local Time Step      4.2278e-08                        280409


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.68428          2.4558         0.18359        0.050504
v  Velocity[Y]             -1.9371          3.0935         0.15804         0.11673
v  Velocity[Z]             -3.4446          2.6798       -0.054399      -0.0031944
v  ǁVelocityǁ           0.00028598          4.0827         0.55561         0.93334
v  Pressure                -567.29            5251          3618.5          2870.2
v  k                    2.2718e-16         0.37817       0.0010208       0.0040947
v  epsilon               1.774e-13          80a  Local Time Step      4.2278e-08                        280409


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.68428          2.4558         0.18359        0.050504
v  Velocity[Y]             -1.9371          3.0935         0.15804         0.11673
v  Velocity[Z]             -3.4446          2.6798       -0.054399      -0.0031944
v  ǁVelocityǁ           0.00028598          4.0827         0.55561         0.93334
v  Pressure                -567.29            5251          3618.5          2870.2
v  k                    2.2718e-16         0.37817       0.0010208       0.0040947
v  epsilon               1.774e-13          8071.1          1.4831          1.2055
v  TurbVisc             3.9661e-22         0.11236        0.001854       0.0042433
v  CourantNb            0.00085318           60732          31.136          9.5174
v  FourierNb               0.21899      2.3653e+06          218.87          2.8198
v  total_pressure       4.9943e+05      5.0525e+05      5.0362e+05      5.0287e+05
v  Local Time Step            0.01        0.020857         0.01001        0.010032


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.1549       2.426e+06          250.01          12.337


 TIME FOR THE TIME STEP                6:        0.23517E+03

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


 INSTANT    0.700000000E+00   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        -0.147007758E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491654E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.47338E+00 0.15492E+01
   Friction velocity        uet   :  0.12674E-01 0.25349E+02
   Friction velocity        uk    :  0.12673E-01 0.25349E+02
   Dimensionless distance   yplus :  0.31028E-02 0.74902E+01
   ------------------------------------------------------
   Nb of reversal of tha  Local Time Step      4.2278e-08                        280409


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.68428          2.4558         0.18359        0.050504
v  Velocity[Y]             -1.9371          3.0935         0.15804         0.11673
v  Velocity[Z]             -3.4446          2.6798       -0.054399      -0.0031944
v  ǁVelocityǁ           0.00028598          4.0827         0.55561         0.93334
v  Pressure                -567.29            5251          3618.5          2870.2
v  k                    2.2718e-16         0.37817       0.0010208       0.0040947
v  epsilon               1.774e-13          8071.1          1.4831          1.2055
v  TurbVisc             3.9661e-22         0.11236        0.001854       0.0042433
v  CourantNb            0.00085318           60732          31.136          9.5174
v  FourierNb               0.21899      2.3653e+06          218.87          2.8198
v  total_pressure       4.9943e+05      5.0525e+05      5.0362e+05      5.0287e+05
v  Local Time Step            0.01        0.020857         0.01001        0.010032


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.1549       2.426e+06          250.01          12.337


 TIME FOR THE TIME STEP                6:        0.22741E+03

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


 INSTANT    0.700000000E+00   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        -0.147007758E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491654E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.47338E+00 0.15492E+01
   Friction velocity        uet   :  0.12674E-01 0.25349E+02
   Friction velocity        uk    :  0.12673E-01 0.25349E+02
   Dimensionless distance   yplus :  0.31028E-02 0.74902E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        430
   Nb of faces within the viscous sub-layer     :      34774
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24092E+00     454   0.10166E+00   0.40105E+00 0.63103E+01 
c  Velo   Nb of reversal of the velocity at the wall   :        454
   Nb of faces within the viscous sub-layer     :      34673
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24516E+00     440   0.10678E+00   0.35334E+00 0.58599E+01 
c  Velocity[X]                                      0.79585E-01 
c  Velocity[Y]                                      0.13100E+00 
c  Velocity[Z]                                      0.14275E+00 
c  Pressure     0.435   Nb of reversal of the velocity at the wall   :        454
   Nb of faces within the viscous sub-layer     :      34673
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24516E+00     440   0.10678E+00   0.35334E+00 0.58599E+01 
c  Velocity[X]                                      0.79585E-01 
c  Velocity[Y]                                      0.13100E+00 
c  Velocity[Z]                                      0.14275E+00 
c  Pressure     0.43596E-01    1592   0.17486E+00   0.31028E+00 0.56655E+01 
c  k            0.71121E-02     300   0.12703E-02   0.66131E-04 0.93278E+01 
c  epsilon      0.67805E+02     129   0.76624E-03   0.26526E+04 0.46440E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.5965e-05                            46
a  epsilon                -0.10971                            76
a  Local Time Step      4.2278e-08                        280268


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

   field                   minimum         maximum        se   Nb of reversal of the velocity at the wall   :        454
   Nb of faces within the viscous sub-layer     :      34673
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24516E+00     440   0.10678E+00   0.35334E+00 0.58599E+01 
c  Velocity[X]                                      0.79585E-01 
c  Velocity[Y]                                      0.13100E+00 
c  Velocity[Z]                                      0.14275E+00 
c  Pressure     0.43596E-01    1592   0.17486E+00   0.31028E+00 0.56655E+01 
c  k            0.71121E-02     300   0.12703E-02   0.66131E-04 0.93278E+01 
c  epsilon      0.67805E+02     129   0.76624E-03   0.26526E+04 0.46440E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.5965e-05                            46
a  epsilon                -0.10971                            76
a  Local Time Step      4.2278e-08                        280268


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

   field                   minimum         maximum        se   Nb of reversal of the velocity at the wall   :        454
   Nb of faces within the viscous sub-layer     :      34673
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24516E+00     440   0.10678E+00   0.35334E+00 0.58599E+01 
c  Velocity[X]                                      0.79585E-01 
c  Velocity[Y]                                      0.13100E+00 
c  Velocity[Z]                                      0.14275E+00 
c  Pressure     0.43596E-01    1592   0.17486E+00   0.31028E+00 0.56655E+01 
c  k            0.71121E-02     300   0.12703E-02   0.66131E-04 0.93278E+01 
c  epsilon      0.67805E+02     129   0.76624E-03   0.26526E+04 0.46440E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.5965e-05                            46
a  epsilon                -0.10971                            76
a  Local Time Step      4.2278e-08                        280268


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.8277          2.3667         0.19294        0.050375
v  Velocity[Y]             -2.0171          3.3219         0.15282         0.11894
v  Velocity[Z]              -3.513          2.7362       -0.058951     -0.00050303
v  ǁVelocityǁ            0.0005106          4.0852          0.5866         0.95208
v  Pressure                -64.325          6361.9          4366.8          3553.3
v  k                    1.6762e-11         0.32909       0.0011962       0.0043016
v  epsilon              8.7717e-11          6670.5          1.6194          1.2941
v  TurbVisc             1.3972e-18         0.11246       0.0013014       0.0043337
v  CourantNb             0.0013669           66409           33.26          9.7759
v  FourierNb               0.21983      2.3653e+06          218.46          2.7885
v  total_pressure       4.9994e+05      5.0636e+05      5.0437e+05      5.0355e+05
v  Local Time Step            0.01        0.025237        0.010016         0.01006


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.3052      2.4317e+06          251.72          12.564


 TIME FOR THE TIME STEP                8:        0.21316E+03

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


 INSTANT    0.900000000E+00   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         0.159561970E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491652E+00
Free inlet               13           0       

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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.108696527E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491644E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00

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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.108696527E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491644E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52378E+00 0.13005E+01
   Friction velocity        uet   :  0.61335E-02 0.33214E+02
   Friction velocity        uk    :  0.61325E-02 0.33214E+02
   Dimensionless distance   yplus :  0.42382E-02 0.76174E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        507
   Nb of faces within the viscous sub-layer     :      34509
   Total number of wall faces                   :      41000
---------------------

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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.108696527E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491644E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52378E+00 0.13005E+01
   Friction velocity        uet   :  0.61335E-02 0.33214E+02
   Friction velocity        uk    :  0.61325E-02 0.33214E+02
   Dimensionless distance   yplus :  0.42382E-02 0.76174E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        507
   Nb of faces within the viscous sub-layer     :      34509
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24642E+00     435   0.11465E+00   0.26906E+00 0.50532E+01 
c  Velocity[X]                                      0.54015E-01 
c  Velocity[Y]                                      0.90471E-01 
c  Velocity[Z]                                      0.12458E+00 
c  Pressure     0.38596E-01    1374   0.12759E+00   0.24078E+00 0.14292E+01 
c  k            0.70284E-02     300   0.11584E-02   0.51867E-04 0.81632E+01 
c  epsilon      0.35787E+02     139   0.24964E-02   0.39840E+04 0.67124E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.2289e-05                            19
a  epsilon                -0.38037                            25
a  Local Time Step      4.2278e-08                        280441


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -0.981          2.3594         0.19846        0.050172
v  Velocity[Y]             -2.1575           3.328         0.15189         0.12003
v  Velocity[Z]             -3.5752          2.7564       -0.074301      -0.0005288
v  ǁVelocityǁ            0.0001828          4.0509         0.61923          0.9643
v  Pressure                -136.92          6558.3          4501.5          3650.9
v  k                    1.1305e-09         0.24508       0.0013259       0.0044213
v  epsilon              3.4732e-07          4058.6           1.728          1.3683
v  TurbVisc             1.4276e-14          0.1125      0.00096987       0.0043802
v  CourantNb             0.0014998           56903          34.979          10.006
v  FourierNb               0.22037      2.3653e+06          218.09          2.7739
v  total_pressure       4.9986e+05      5.0656e+05       5.045e+05      5.0365e+05
v  Local Time Step            0.01        0.030537        0.010019        0.010093


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.1555      2.4211e+06          253.07           12.78


 TIME FOR THE TIME STEP               10:        0.19667E+03

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


 INSTANT    0.110000000E+01   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         0.208381208E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491641E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.v  Velocity[Y]             -2.1843          3.3877         0.15099         0.11998
v  Velocity[Z]              -3.638          2.7688       -0.081924     -0.00069685
v  ǁVelocityǁ           0.00043648          4.0477         0.63516         0.96816
v  Pressure                 -156.2          6643.3          4551.8          3698.2
v  k                    1.4059e-09         0.12883       0.0013876       0.0044587
v  epsilon              4.8543e-07          948.54           1.782           1.397
v  TurbVisc             1.5307e-14         0.11251      0.00087306       0.0043911
v  CourantNb             0.0018249           57827          35.921          10.112
v  FourierNb               0.22054      2.3653e+06          217.95          2.7699
v  total_pressure       4.9984e+05      5.0664e+05      5.0455e+05       5.037e+05
v  Localv  Velocity[Y]             -2.1843          3.3877         0.15099         0.11998
v  Velocity[Z]              -3.638          2.7688       -0.081924     -0.00069685
v  ǁVelocityǁ           0.00043648          4.0477         0.63516         0.96816
v  Pressure                 -156.2          6643.3          4551.8          3698.2
v  k                    1.4059e-09         0.12883       0.0013876       0.0044587
v  epsilon              4.8543e-07          948.54           1.782           1.397
v  TurbVisc             1.5307e-14         0.11251      0.00087306       0.0043911
v  CourantNb             0.0018249           57827          35.921          10.112
v  FourierNb               0.22054      2.3653e+06          217.95          2.7699
v  total_pressure       4.9984e+05      5.0664e+05      5.0455e+05       5.037e+05
v  Local Time Step            0.01         0.03359         0.01002        0.010102


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.1549      2.4168e+06          253.88          12.882


 TIME FOR THE TIME STEP               11:        0.19496E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass v  Velocity[Y]             -2.1843          3.3877         0.15099         0.11998
v  Velocity[Z]              -3.638          2.7688       -0.081924     -0.00069685
v  ǁVelocityǁ           0.00043648          4.0477         0.63516         0.96816
v  Pressure                 -156.2          6643.3          4551.8          3698.2
v  k                    1.4059e-09         0.12883       0.0013876       0.0044587
v  epsilon              4.8543e-07          948.54           1.782           1.397
v  TurbVisc             1.5307e-14         0.11251      0.00087306       0.0043911
v  CourantNb             0.0018249           57827          35.921          10.112
v  FourierNb               0.22054      2.3653e+06          217.95          2.7699
v  total_pressure       4.9984e+05      5.0664e+05      5.0455e+05       5.037e+05
v  Local Time Step            0.01         0.03359         0.01002        0.010102


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.1549      2.4168e+06          253.88          12.882


 TIME FOR THE TIME STEP               11:        0.20835E+03

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


 INSTANT    0.120000000E+01   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         0.215407774E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491643E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51296E+00 0.88910E+00
   Friction velocity        uet   :  0.98987E-02 0.32211E+02
   Friction velocity        uk    :  0.98739E-02 0.32211E+02
   Dimensionless distance   yplus :  0.41101E-02 0.75660E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        538
   Nb of faces within the viscous sub-layer     :      34311
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24542E+00     428   0.11615E+00   0.18692E+00 0.41868E+01 
c  Velocity[X]                                      0.34024E-01 
c  Velocity[Y]                                      0.74050E-01 
c  Velocity[Z]                                      0.78848E-01 
c  Pressure     0.32692E-01    1390   0.96973E-01   0.18669E+00 0.14983E+01 
c  k            0.70533E-02     294   0.82324E-03   0.42582E-04 0.73319E+01 
c  epsilon      0.19062E+02     164   0.17291E-02   0.59535E+03 0.26757E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.1897e-05                             9
a  epsilon               -0.036757                            11
a  Local Time Step      4.2278e-08                        280471


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0786          2.3599         0.20463        0.050117
v  Velocity[Y]             -2.2089          3.4066         0.14933         0.11986
v  Velocity[Z]             -3.7089          2.7487       -0.088202     -0.00072311
v  ǁVelocityǁ           0.00025589           4.087         0.64903         0.97161
v  Pressure                -152.91          6744.1          4610.7          3754.5
v  k                    1.8824e-09         0.16787       0.0014626       0.0044913
v  epsilon              7.5104e-07            1225          1.9023          1.4337
v  TurbVisc             1.6674e-14         0.11252      0.00079733       0.0043959
v  CourantNb            0.00020986           56069          36.807          10.212
v  FourierNb               0.22067      2.3653e+06          217.84          2.7661
v  total_pressure       4.9985e+05      5.0674e+05      5.0461e+05      5.0375e+05
v   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24555E+00     424   0.11907E+00   0.15453E+00 0.37971E+01 
c  Velocity[X]                                      0.28986E-01 
c  Velocity[Y]                                      0.62629E-01 
c  Velocity[Z]                                      0.62916E-01 
c  Pressure     0.29639E-01    1377   0.84474E-01   0.16394E+00 0.12893E+01 
c  k            0.71024E-02     287   0.62859E-03   0.30473E-04 0.61851E+01 
c  epsilon      0.19494E+02     149   0.12743E-02   0.46444E+03 0.23423E+02 
-----------------------------------------------------------------------------
  
  

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

   field               in   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24555E+00     424   0.11907E+00   0.15453E+00 0.37971E+01 
c  Velocity[X]                                      0.28986E-01 
c  Velocity[Y]                                      0.62629E-01 
c  Velocity[Z]                                      0.62916E-01 
c  Pressure     0.29639E-01    1377   0.84474E-01   0.16394E+00 0.12893E+01 
c  k            0.71024E-02     287   0.62859E-03   0.30473E-04 0.61851E+01 
c  epsilon      0.19494E+02     149   0.12743E-02   0.46444E+03 0.23423E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0003027                            27
a  epsilon                 -2.4723                            30
a  Local Time Step      4.2278e-08                        280548


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0895          2.3751         0.20766        0.050257
v  Velocity[Y]             -2.2241          3.5053         0.14707         0.11977
v  Velocity[Z]             -3.7662          2.7238       -0.092936     -0.00065751
v  ǁVelocityǁ           0.00018248   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24555E+00     424   0.11907E+00   0.15453E+00 0.37971E+01 
c  Velocity[X]                                      0.28986E-01 
c  Velocity[Y]                                      0.62629E-01 
c  Velocity[Z]                                      0.62916E-01 
c  Pressure     0.29639E-01    1377   0.84474E-01   0.16394E+00 0.12893E+01 
c  k            0.71024E-02     287   0.62859E-03   0.30473E-04 0.61851E+01 
c  epsilon      0.19494E+02     149   0.12743E-02   0.46444E+03 0.23423E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0003027                            27
a  epsilon                 -2.4723                            30
a  Local Time Step      4.2278e-08                        280548


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0895          2.3751         0.20766        0.050257
v  Velocity[Y]             -2.2241          3.5053         0.14707         0.11977
v  Velocity[Z]             -3.7662          2.7238       -0.092936     -0.00065751
v  ǁVelocityǁ           0.00018248          4.1389         0.66073         0.97494
v  Pressure                -140.73          6834.8          4664.8          3804.2
v  k                    1.8203e-09          0.1558       0.0015009        0.004514
v  epsilon              1.4464e-06          1108.5           1.948          1.4549
v  TurbVisc             2.6018e-14         0.11253      0.00074497       0.0043982
v  CourantNb             0.0022101           54048          37.612          10.296
v  FourierNb               0.22078      2.3653e+06          217.78          2.7638
v  total_pressure       4.9986e+05      5.0683e+05      5.0466e+05       5.038e+05
v  Local Time Step            0.01        0.040644        0.010019        0.010099


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.3332      2.4095e+06          255.39           13.06


 TIME FOR THE TIME STEP               13:        0.20444E+03

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


 INSTANT    0.140000000E+01   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        -0.239877579E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491629E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46375E+00 0.88598E+00
   Friction velocity        uet   :  0.55591E-02 0.29620E+02
   Friction velocity        uk    :  0.55589E-02 0.29620E+02
   Dimensionless distance   yplus :  0.37795E-02 0.74035E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        560
   Nb of faces within the viscous sub-layer     :      34151
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24562E+00     421   0.11657E+00   0.12621E+00 0.34240E+01 
c  Velocity[X]                                      0.24045E-01 
c  Velocity[Y]                                      0.51610E-01 
c  Velocity[Z]                                      0.50553E-01 
c  Pressure     0.27111E-01    1301   0.73775E-01   0.14615E+00 0.99143E+00 
c  k            0.71291E-02     279   0.57383E-03   0.25832E-04 0.56781E+01 
c  epsilon      0.19644E+02     173   0.64663E-03   0.30584E+03 0.18926E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fSmooth wall               5       41000        -0.201151685E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491635E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------Smooth wall               5       41000        -0.201151685E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491635E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43574E+00 0.88278E+00
   Friction velocity        uet   :  0.33294E-02 0.27933E+02
   Friction velocity        uk    :  0.33289E-02 0.27933E+02
   Dimensionless distance   yplus :  0.35642E-02 0.73116E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        565
   Nb of faces within the viscous sub-layer     :      34101
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
----------------------------------------------------------------Smooth wall               5       41000        -0.201151685E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491635E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43574E+00 0.88278E+00
   Friction velocity        uet   :  0.33294E-02 0.27933E+02
   Friction velocity        uk    :  0.33289E-02 0.27933E+02
   Dimensionless distance   yplus :  0.35642E-02 0.73116E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        565
   Nb of faces within the viscous sub-layer     :      34101
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24584E+00     417   0.11672E+00   0.10358E+00 0.30966E+01 
c  Velocity[X]                                      0.21924E-01 
c  Velocity[Y]                                      0.42305E-01 
c  Velocity[Z]                                      0.39353E-01 
c  Pressure     0.24833E-01    1302   0.64935E-01   0.13098E+00 0.69801E+00 
c  k            0.71517E-02     245   0.50863E-03   0.20886E-04 0.51012E+01 
c  epsilon      0.19764E+02     159   0.96018E-03   0.23947E+03 0.16601E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.4934e-05                            28
a  epsilon               -0.038667                            21
a  Local Time Step      4.2278e-08                        280567


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.1136          2.4419         0.21295        0.050762
v  Velocity[Y]             -2.2227          3.5501         0.14357         0.11996
v  Velocity[Z]             -3.8214          2.7126       -0.098823     -0.00045636
v  ǁVelocityǁ           0.00020258          4.1909         0.67833         0.98027
v  Pressure                -125.13          6991.1          4739.5          3868.2
v  k                    6.9369e-10         0.14351       0.0015667       0.0045472
v  epsilon              4.7346e-06          1044.9          2.0208          1.4852
v  TurbVisc             2.5216e-14         0.11253      0.00064003        0.004393
v  CourantNb            0.00092546           44438          38.785          10.428
v  FourierNb               0.22099      2.3653e+06          217.66          2.7578
v  total_pressure       4.9987e+05      5.0699e+05      5.0474e+05      5.0387e+05
v  Local Time Step            0.01        0.045066        0.010019        0.010095


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5534      2.4022e+06          256.44          13.186


 TIME FOR THE TIME STEP               15:        0.18666E+03

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


 INSTANT    0.160000000E+01   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        -0.179765511E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491630E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
----------------------------------------------v  k                    1.1671e-09         0.16892       0.0015966       0.0045591
v  epsilon              4.8587e-06          1333.9          2.1033          1.5005
v  TurbVisc             3.3196e-15         0.11253      0.00058609       0.0043895
v  CourantNb              0.015083           38032          39.165          10.478
v  FourierNb               0.22112      2.3653e+06          217.58          2.7547
v  total_pressure       4.9987e+05      5.0704e+05      5.0476e+05      5.0388e+05
v  Local Time Step            0.01        0.049573        0.010019        0.010096


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.v  k                    1.1671e-09         0.16892       0.0015966       0.0045591
v  epsilon              4.8587e-06          1333.9          2.1033          1.5005
v  TurbVisc             3.3196e-15         0.11253      0.00058609       0.0043895
v  CourantNb              0.015083           38032          39.165          10.478
v  FourierNb               0.22112      2.3653e+06          217.58          2.7547
v  total_pressure       4.9987e+05      5.0704e+05      5.0476e+05      5.0388e+05
v  Local Time Step            0.01        0.049573        0.010019        0.010096


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7135      2.3989e+06          256.75          13.233


 TIME FOR THE TIME STEP               16:        0.18148E+03

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


 INSTANT    0.170000000E+01   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        -0.102785634E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlv  k                    1.1671e-09         0.16892       0.0015966       0.0045591
v  epsilon              4.8587e-06          1333.9          2.1033          1.5005
v  TurbVisc             3.3196e-15         0.11253      0.00058609       0.0043895
v  CourantNb              0.015083           38032          39.165          10.478
v  FourierNb               0.22112      2.3653e+06          217.58          2.7547
v  total_pressure       4.9987e+05      5.0704e+05      5.0476e+05      5.0388e+05
v  Local Time Step            0.01        0.049573        0.010019        0.010096


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7135      2.3989e+06          256.75          13.233


 TIME FOR THE TIME STEP               16:        0.18092E+03

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


 INSTANT    0.170000000E+01   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        -0.102785634E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491623E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40885E+00 0.87825E+00
   Friction velocity        uet   :  0.76348E-02 0.23559E+02
   Friction velocity        uk    :  0.76203E-02 0.23559E+02
   Dimensionless distance   yplus :  0.30061E-02 0.72193E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        564
   Nb of faces within the viscous sub-layer     :      33990
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24622E+00     409   0.11879E+00   0.70611E-01 0.25501E+01 
c  Velocity[X]                                      0.16040E-01 
c  Velocity[Y]                                      0.28225E-01 
c  Velocity[Z]                                      0.26346E-01 
c  Pressure     0.20823E-01    1085   0.51128E-01   0.10623E+00 0.24631E+00 
c  k            0.71879E-02     244   0.51163E-03   0.17720E-04 0.46855E+01 
c  epsilon      0.20061E+02     129   0.94003E-03   0.21851E+03 0.15625E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00061207                            21
a  epsilon                -0.72338                            19
a  Local Time Step      4.2278e-08                        280576


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.1477          2.4399         0.21723        0.050894
v  Velocity[Y]             -2.2211          3.3107         0.14207         0.11999
v  Velocity[Z]             -3.8614           2.683        -0.10242     -0.00027868
v  ǁVelocityǁ           0.00058594          4.2394           0.691         0.98373
v  Pressure                -143.17            7069          4763.5            3889
v  k                    2.0771e-09         0.14622       0.0015923       0.0045665
v  epsilon              6.7355e-06          879.93          2.0813          1.5086
v  TurbVisc             1.7693e-14         0.11253       0.0005376       0.0043859
v  CourantNb            0.00092109           32858          39.504          10.519
v  FourierNb               0.22127      2.3653e+06          217.51          2.7534
v  total_pressure       4.9986e+05      5.0707e+05      5.0476e+05      5.0389e+05
v  Local Time Step            0.01         0.05453        0.010019          0.0101


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --c  Velocity[Y]                                      0.25811E-01 
c  Velocity[Z]                                      0.22173E-01 
c  Pressure     0.18974E-01     958   0.45394E-01   0.95523E-01 0.18302E+00 
c  k            0.71967E-02     244   0.44533E-03   0.18166E-04 0.47406E+01 
c  epsilon      0.20118E+02     134   0.54643E-03   0.20181E+03 0.14923E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.8181e-06                             8
a  epsilon               -0.015296                            11
a  Local Time Step      4.2278e-08 c  Velocity[Y]                                      0.25811E-01 
c  Velocity[Z]                                      0.22173E-01 
c  Pressure     0.18974E-01     958   0.45394E-01   0.95523E-01 0.18302E+00 
c  k            0.71967E-02     244   0.44533E-03   0.18166E-04 0.47406E+01 
c  epsilon      0.20118E+02     134   0.54643E-03   0.20181E+03 0.14923E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.8181e-06                             8
a  epsilon               -0.015296                            11
a  Local Time Step      4.2278e-08                        280591


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.1614          2.4405         0.21863        0.050756
v  Velocity[Y]             -2.2253          3.2286         0.14191         0.11996
v  Velocity[Z]             -3.8799          2.6737        -0.10395     -0.00034002
v  ǁVelocityǁ           0.00055721          4.2488         0.69593         0.98503
v  Pressure                -159.03          7090.2          4766.1          3892.5
v  k                    2.2009e-09         0.16386       0.0016171        0.004573
v  epsilon              6.0148e-06          1118.4          2.1461          1.5165
c  Velocity[Y]                                      0.25811E-01 
c  Velocity[Z]                                      0.22173E-01 
c  Pressure     0.18974E-01     958   0.45394E-01   0.95523E-01 0.18302E+00 
c  k            0.71967E-02     244   0.44533E-03   0.18166E-04 0.47406E+01 
c  epsilon      0.20118E+02     134   0.54643E-03   0.20181E+03 0.14923E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.8181e-06                             8
a  epsilon               -0.015296                            11
a  Local Time Step      4.2278e-08                        280591


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.1614          2.4405         0.21863        0.050756
v  Velocity[Y]             -2.2253          3.2286         0.14191         0.11996
v  Velocity[Z]             -3.8799          2.6737        -0.10395     -0.00034002
v  ǁVelocityǁ           0.00055721          4.2488         0.69593         0.98503
v  Pressure                -159.03          7090.2          4766.1          3892.5
v  k                    2.2009e-09         0.16386       0.0016171        0.004573
v  epsilon              6.0148e-06          1118.4          2.1461          1.5165
v  TurbVisc             2.1764e-14         0.11253      0.00049695        0.004382
v  CourantNb              0.015591           29048          39.755          10.553
v  FourierNb                0.2214      2.3653e+06          217.44          2.7523
v  total_pressure       4.9984e+05      5.0709e+05      5.0477e+05      5.0389e+05
v  Local Time Step            0.01        0.059983         0.01002        0.010106


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7131      2.3943e+06           257.2          13.305


 TIME FOR THE TIME STEP               18:        0.16540E+03

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


 INSTANT    0.190000000E+01   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        -0.331617470E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491630E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39946E+00 0.88870E+00
   Friction velocity        uet   :  0.11891E-01 0.19120E+02
   Friction velocity        uk    :  0.11890E-01 0.19120E+02
   Dimensionless distance   yplus :  0.24397E-02 0.71879E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        557
   Nb of faces within the viscous sub-layer     :      33909
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24638E+00     398   0.11886E+00   0.56914E-01 0.22855E+01 
c  Velocity[X]                                      0.12977E-01 
c  Velocity[Y]                                      0.24075E-01 
c  Velocity[Z]                                      0.19862E-01 
c  Pressure     0.17956E-01    1098   0.41489E-01   0.89501E-01 0.17550E+00 
c  k            0.71999E-02     238   0.52588E-03   0.12840E-04 0.39831E+01 
c  epsilon      0.20129E+02     138   0.95263E-03   0.12969E+03 0.11943E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -5.879e-06                             9
a  epsilon                -0.02713                     Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39590E+00 0.89011E+00
   Friction velocity        uet   :  0.13741E-01 0.16431E+02
   Friction velocity        uk    :  0.13730E-01 0.16431E+02
   Dimensionless distance   yplus :  0.20967E-02 0.71766E+01
   ------------------------------------------------------
   Nb of reConvective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39590E+00 0.89011E+00
   Friction velocity        uet   :  0.13741E-01 0.16431E+02
   Friction velocity        uk    :  0.13730E-01 0.16431E+02
   Dimensionless distance   yplus :  0.20967E-02 0.71766E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        549
   Nb of faces within the viscous sub-layer     :      33881
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24660E+00     394   0.11984E+00   0.54096E-01 0.22267E+01 
c  Velocity[X]                                      0.12551E-01 
c  Velocity[Y]                                      0.23693E-01 
c  Velocity[Z]                                      0.17852E-01 
c  Pressure     0.16571E-01    114Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39590E+00 0.89011E+00
   Friction velocity        uet   :  0.13741E-01 0.16431E+02
   Friction velocity        uk    :  0.13730E-01 0.16431E+02
   Dimensionless distance   yplus :  0.20967E-02 0.71766E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        549
   Nb of faces within the viscous sub-layer     :      33881
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24660E+00     394   0.11984E+00   0.54096E-01 0.22267E+01 
c  Velocity[X]                                      0.12551E-01 
c  Velocity[Y]                                      0.23693E-01 
c  Velocity[Z]                                      0.17852E-01 
c  Pressure     0.16571E-01    1148   0.37097E-01   0.81927E-01 0.24703E+00 
c  k            0.72106E-02     229   0.48788E-03   0.20462E-04 0.50218E+01 
c  epsilon      0.20266E+02     122   0.79441E-03   0.34603E+03 0.19268E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00027111                            36
a  epsilon                 -1.8688                            55
a  Local Time Step      4.2278e-08                        280621


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.2064          2.4163         0.22132        0.050439
v  Velocity[Y]              -2.238          3.2183         0.14128         0.11984
v  Velocity[Z]             -3.9174          2.6524        -0.10553     -0.00047336
v  ǁVelocityǁ           0.00027893          4.2941         0.70283         0.98709
v  Pressure                 -207.3          7090.6          4743.9          3879.9
v  k                    2.0949e-09         0.16572       0.0016136       0.0045816
v  epsilon              5.3466e-07          1101.1          2.1673          1.5315
v  TurbVisc             2.0165e-14         0.11253      0.00043657        0.004375
v  CourantNb            0.00072644           26435          40.138          10.603
v  FourierNb               0.22155      2.3653e+06          217.35          2.7504
v  total_pressure       4.9979e+05      5.0709e+05      5.0474e+05      5.0388e+05
v  Local Time Step            0.01         0.07258        0.010021        0.010122


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7301      2.3917e+06          257.49          13.353


 TIME FOR THE TIME STEP               20:        0.16467E+03

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


 INSTANT    0.210000000E+01   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         0.247942014E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491781E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39507E+00 0.89416E+00
   Friction velocity        uet   :  0.76536E-02 0.14987E+02
   Friction velocity        uk    :  0.76511E-02 0.14987E+02
   Dimensionless distance   yplus :  0.19072E-02 0.v  CourantNb             0.0065808           23257          40.241           10.62
v  FourierNb               0.22159      2.3653e+06          217.32          2.7503
v  total_pressure       4.9976e+05      5.0708e+05      5.0473e+05      5.0387e+05
v  Local Time Step            0.01        0.079838        0.010022        0.010131


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7367       2.388e+06          257.56          13.371


 TIME FOR THE TIME STEP               21:        0.17398E+03

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


 INSTANT    0.220000000E+01   TIME STEP NUMBER              22
 ==v  CourantNb             0.0065808           23257          40.241           10.62
v  FourierNb               0.22159      2.3653e+06          217.32          2.7503
v  total_pressure       4.9976e+05      5.0708e+05      5.0473e+05      5.0387e+05
v  Local Time Step            0.01        0.079838        0.010022        0.010131


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7367       2.388e+06          257.56          13.371


 TIME FOR THE TIME STEP               21:        0.17365E+03

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


 INSTANT    0.220000000E+01   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        -0.271480577E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491788E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Unv  CourantNb             0.0065808           23257          40.241           10.62
v  FourierNb               0.22159      2.3653e+06          217.32          2.7503
v  total_pressure       4.9976e+05      5.0708e+05      5.0473e+05      5.0387e+05
v  Local Time Step            0.01        0.079838        0.010022        0.010131


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7367       2.388e+06          257.56          13.371


 TIME FOR THE TIME STEP               21:        0.17457E+03

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


 INSTANT    0.220000000E+01   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        -0.271480577E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491788E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37746E+00 0.88829E+00
   Friction velocity        uet   :  0.76756E-02 0.14639E+02
   Friction velocity        uk    :  0.76558E-02 0.14639E+02
   Dimensionless distance   yplus :  0.18679E-02 0.71168E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        550
   Nb of faces within the viscous sub-layer     :      33830
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24668E+00     383   0.11959E+00   0.51893E-01 0.21793E+01 
c  Velocity[X]                                      0.11488E-01 
c  Velocity[Y]                                      0.23378E-01 
c  Velocity[Z]                                      0.17027E-01 
c  Pressure     0.15518E-01    1205   0.32239E-01   0.75890E-01 0.31826E+00 
c  k            0.72186E-02     209   0.36799E-03   0.10415E-04 0.35824E+01 
c  epsilon      0.20378E+02     121   0.92880E-03   0.12692E+03 0.11733E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.7967e-06                            11
a  epsilon               -0.011724                             8
a  Local Time Step      4.2278e-08                        280657


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -1.231          2.3522         0.22307        0.050234
v  Velocity[Y]             -2.2568          3.2145         0.14099         0.11971
v  Velocity[Z]              -4.165           2.633         -0.1068     -0.00045489
v  ǁVelocityǁ             0.000308          4.5134         0.70737         0.98821
v  Pressure                 -274.5          7061.1          4705.8          3856.9
v  k                    2.1046e-09         0.15328       0.0016028       0.0045835
v  epsilon              9.2219e-06          1001.6          2.1791          1.5348
v  TurbVisc             1.9155e-14         0.11253      0.00040041       0.0043714
v  CourantNb             0.0036305           23340           40.32          10.633
v  FourierNb                0.2216      2.3653e+06          217.29          2.7507
v  total_pressure       4.9973e+05      5.0706e+05      5.0471e+05      5.0386e+05
v  Local Time Step            0.01        0.087822        0.010023        0.010139


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7421      2.3858e+06          257.61          13.384


 TIME FOR THE TIME STEP               22:        0.16886E+03

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


 INSTANT    0.230000000E+01   TIME STEP NUMBER            c  epsilon      0.20448E+02     114   0.66984E-03   0.89995E+02 0.98343E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.1772e-06                            10
a  epsilon              -0.0062465                             6
a  Local Time Step      4.2278e-08                        280672


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]           c  epsilon      0.20448E+02     114   0.66984E-03   0.89995E+02 0.98343E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.1772e-06                            10
a  epsilon              -0.0062465                             6
a  Local Time Step      4.2278e-08                        280672


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.2335          2.3098         0.22397        0.050121
v  Velocity[Y]              -2.253          3.0758         0.14121         0.11963
v  Velocity[Z]             -4.0146          2.6308        -0.10793     -0.00049529
v  ǁVelocityǁ           0.00048385          4.3763          0.7097         0.98853
v  Pressure                -302.06            7043          4686.8          3845.6
v  k                    2.1293e-09         0.15708       0.0016063       0.0045875
v  epsilon              1.0125e-05          1039.1          2.1962          1.5412
v  TurbVisc             1.9816e-14         0.11253       0.0003883       0.0043698
v  CourantNb             0.0047469           23530          40.448          10.645
v  FourierNb               0.22161      2.3653e+06          217.27          2.7507
v  total_pressure        4.997e+05 c  epsilon      0.20448E+02     114   0.66984E-03   0.89995E+02 0.98343E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.1772e-06                            10
a  epsilon              -0.0062465                             6
a  Local Time Step      4.2278e-08                        280672


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.2335          2.3098         0.22397        0.050121
v  Velocity[Y]              -2.253          3.0758         0.14121         0.11963
v  Velocity[Z]             -4.0146          2.6308        -0.10793     -0.00049529
v  ǁVelocityǁ           0.00048385          4.3763          0.7097         0.98853
v  Pressure                -302.06            7043          4686.8          3845.6
v  k                    2.1293e-09         0.15708       0.0016063       0.0045875
v  epsilon              1.0125e-05          1039.1          2.1962          1.5412
v  TurbVisc             1.9816e-14         0.11253       0.0003883       0.0043698
v  CourantNb             0.0047469           23530          40.448          10.645
v  FourierNb               0.22161      2.3653e+06          217.27          2.7507
v  total_pressure        4.997e+05      5.0704e+05      5.0469e+05      5.0385e+05
v  Local Time Step            0.01        0.096604        0.010024        0.010147


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7325      2.3844e+06          257.72          13.395


 TIME FOR THE TIME STEP               23:        0.16860E+03

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


 INSTANT    0.240000000E+01   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        -0.439849061E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491790E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36743E+00 0.89191E+00
   Friction velocity        uet   :  0.52465E-02 0.15003E+02
   Friction velocity        uk    :  0.52451E-02 0.15003E+02
   Dimensionless distance   yplus :  0.19144E-02 0.70848E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        549
   Nb of faces within the viscous sub-layer     :      33785
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24668E+00     373   0.12164E+00   0.45989E-01 0.20505E+01 
c  Velocity[X]                                      0.10358E-01 
c  Velocity[Y]                                      0.19769E-01 
c  Velocity[Z]                                      0.15863E-01 
c  Pressure     0.13889E-01    1195   0.28264E-01   0.67435E-01 0.29936E+00 
c  k            0.72210E-02     195   0.35270E-03   0.93594E-05 0.33936E+01 
c  epsilon      0.20414E+02     105   0.61854E-03   0.15632E+03 0.12929E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00055695                            13
a  epsilon               -0.036835                             9
a  Local Time Step      4.2278e-08                        280672


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  ------------   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.35090E+00 0.89732E+00
   Friction velocity        uet   :  0.64515E-02 0.15891E+02
   Friction velocity        uk    :  0.64386E-02 0.15891E+02
   Dimensionless distance   yplus :  0.20277E-02 0.70262E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        549
   Nb of faces within the viscous sub-layer     :      33773
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.35090E+00 0.89732E+00
   Friction velocity        uet   :  0.64515E-02 0.15891E+02
   Friction velocity        uk    :  0.64386E-02 0.15891E+02
   Dimensionless distance   yplus :  0.20277E-02 0.70262E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        549
   Nb of faces within the viscous sub-layer     :      33773
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24651E+00     371   0.12127E+00   0.45273E-01 0.20341E+01 
c  Velocity[X]                                      0.10945E-01 
c  Velocity[Y]                                      0.19222E-01 
c  Velocity[Z]                                      0.15106E-01 
c  Pressure     0.13648E-01    1196   0.27049E-01   0.66187E-01 0.28046E+00 
c  k            0.72212E-02     192   0.30753E-03   0.94030E-05 0.33965E+01 
c  epsilon      0.20419E+02     141   0.37700E-03   0.13461E+03 0.12052E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for    ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.35090E+00 0.89732E+00
   Friction velocity        uet   :  0.64515E-02 0.15891E+02
   Friction velocity        uk    :  0.64386E-02 0.15891E+02
   Dimensionless distance   yplus :  0.20277E-02 0.70262E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        549
   Nb of faces within the viscous sub-layer     :      33773
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24651E+00     371   0.12127E+00   0.45273E-01 0.20341E+01 
c  Velocity[X]                                      0.10945E-01 
c  Velocity[Y]                                      0.19222E-01 
c  Velocity[Z]                                      0.15106E-01 
c  Pressure     0.13648E-01    1196   0.27049E-01   0.66187E-01 0.28046E+00 
c  k            0.72212E-02     192   0.30753E-03   0.94030E-05 0.33965E+01 
c  epsilon      0.20419E+02     141   0.37700E-03   0.13461E+03 0.12052E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012579                            12
a  epsilon                -0.16578                            14
a  Local Time Step      4.2278e-08                        280666


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.2369           2.253         0.22502        0.050033
v  Velocity[Y]             -2.2638          3.0158         0.14258         0.11942
v  Velocity[Z]             -4.0479          2.6149        -0.11025      -0.0005141
v  ǁVelocityǁ           0.00076172          4.4093         0.71407         0.98904
v  Pressure                -344.07          7003.3          4649.5          3823.2
v  k                     2.175e-09         0.15401        0.001607       0.0045878
v  epsilon              1.5824e-05          1010.2          2.1998          1.5422
v  TurbVisc             1.9953e-14         0.11253      0.00037443       0.0043676
v  CourantNb              0.013008           23260          40.752          10.663
v  FourierNb               0.22164      2.3653e+06          217.26          2.7519
v  total_pressure       4.9966e+05        5.07e+05      5.0465e+05      5.0382e+05
v  Local Time Step            0.01         0.11689        0.010026        0.010162


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7657      2.3818e+06          258.01          13.415


 TIME FOR THE TIME STEP               25:        0.16833E+03

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


 INSTANT    0.260000000E+01   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        -0.153975392E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491797E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.34367E+00 0.89959E+00
   Friction velocity        uet   :  0.13582E-01 0.16634E+02
   Friction velocity        uk    :  0.13568E-01 0.16634E+02
   Dimensionless distance   yplus :  0.18623E-02 0.70005E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        553
   Nb of faces within the viscous sub-layer     :      33764
   Total number of wall faces                   :      41000
------------------------------------------------------------



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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7913      2.3807e+06          258.16           13.42


 TIME FOR THE TIME STEP               26:        0.16350E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet
  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7913      2.3807e+06          258.16           13.42


 TIME FOR THE TIME STEP               26:        0.16316E+03

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


 INSTANT    0.270000000E+01   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        -0.405162308E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491797E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.33838E+00 0.89912E+00
   Friction velocity        uet   :  0.86384E-02 0.16463E+02
   Friction velocity        uk    :  0.85703E-02 0.16463E+02
   Dimensionless distance   yplus :  0.13859E-02 0.69817E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        559
   Nb of faces within the viscous sub-layer     :      33761
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24650E+00     359   0.12025E+00   0.43474E-01 0.19933E+01 
c  Velocity[X]                                      0.10597E-01 
c  Velocity[Y]                                      0.17926E-01 
c  Velocity[Z]                                      0.14950E-01 
c  Pressure     0.12684E-01    1158   0.25009E-01   0.61423E-01 0.24295E+00 
c  k            0.72244E-02     177   0.60775E-03   0.73114E-05 0.29986E+01 
c  epsilon      0.20468E+02     100   0.40422E-03   0.72152E+02 0.87930E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.1914e-05                            12
a  epsilon               -0.042834                             8
a  Local Time Step      4.2278e-08                        280661


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.2286          2.2231         0.22541        0.050096
v  Velocity[Y]             -2.2616          2.9867         0.14379         0.11933
v  Velocity[Z]              -4.054          2.6156        -0.11297     -0.00047709
v  ǁVelocityǁ           0.00050429          4.4222         0.71786         0.98906
v  Pressure                -375.09          6968.7          4619.6          3805.6
v  k                    2.2392e-09         0.15435        0.001608        0.004587
v  epsilon               7.269e-06          1019.6          2.2191          1.5459
v  TurbVisc             2.2279e-14         0.11253      0.00036384       0.0043646
v  CourantNb              0.018659           23398          41.074          10.671
v  FourierNb               0.22168      2.3653e+06          217.25          2.7512
v  total_pressure       4.9962e+05      5.0697e+05      5.0462e+05      5.0381e+05
v  Local Time Step            0.01         0.14144        0.010027         0.01017


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7963      2.3822e+06          258.33          13.422


 TIME FOR THE TIME STEP               27:        0.17236E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.970627437E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491795E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.33236E+00 0.89778E+00
   Friction velocity        uet   :  0.10296E-01 0.17086E+02
   Friction velocity        uk    :  0.10288E-01 0.17086E+02
   Dimensionless distance   yplus :  0.14025E-02 0.69590E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        559
   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   -  ---------------  --------------  --------------  ------------  ------------
a  k                    -4.263e-05                             9
a  epsilon               -0.038625                             8
a  Local Time Step      4.2278e-08                        280662


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.2187          2.2049          0.2252        0.050097
v  Velocity[Y]             -2.2644          3.0723         0.14432         0.11936
v  Velocity[Z]             -3.9081          2.6084        -0.11428     -0.00045273
v  ǁVelocityǁ            0.0005964          4.2782         0.71941         0.98906
v  -  ---------------  --------------  --------------  ------------  ------------
a  k                    -4.263e-05                             9
a  epsilon               -0.038625                             8
a  Local Time Step      4.2278e-08                        280662


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.2187          2.2049          0.2252        0.050097
v  Velocity[Y]             -2.2644          3.0723         0.14432         0.11936
v  Velocity[Z]             -3.9081          2.6084        -0.11428     -0.00045273
v  ǁVelocityǁ            0.0005964          4.2782         0.71941         0.98906
v  Pressure                -387.71          6954.4          4607.5          3798.7
v  k                    1.9229e-09         0.15453       0.0016038       0.0045849
v  epsilon              2.0756e-05          1021.1          2.2092          1.5438
v  TurbVisc             1.9795e-14         0.11253      0.00036177        0.004364
v  CourantNb             0.0022618           23224          41.197          10.673
v  FourierNb                0.2217      2.3653e+06          217.25          2.7518
v  total_pressure       4.9961e+05      5.0695e+05      5.0461e+05       5.038e+05
v  Local Time Step            0.01         0.15558        0.010027        0.010171


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.8141       2.381e+06          258.45          13.425


 TIME FOR THE TIME STEP               28:        0.16275E+03

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


 INSTANT    0.290000000E+01   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        -0.289138223E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491793E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32810E+00 0.90154E+00
   Friction velocity        uet   :  0.90933E-02 0.1735-  ---------------  --------------  --------------  ------------  ------------
a  k                    -4.263e-05                             9
a  epsilon               -0.038625                             8
a  Local Time Step      4.2278e-08                        280662


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.2187          2.2049          0.2252        0.050097
v  Velocity[Y]             -2.2644          3.0723         0.14432         0.11936
v  Velocity[Z]             -3.9081          2.6084        -0.11428     -0.00045273
v  ǁVelocityǁ            0.0005964          4.2782         0.71941         0.98906
v  Pressure                -387.71          6954.4          4607.5          3798.7
v  k                    1.9229e-09         0.15453       0.0016038       0.0045849
v  epsilon              2.0756e-05          1021.1          2.2092          1.5438
v  TurbVisc             1.9795e-14         0.11253      0.00036177        0.004364
v  CourantNb             0.0022618           23224          41.197          10.673
v  FourierNb                0.2217      2.3653e+06          217.25          2.7518
v  total_pressure       4.9961e+05      5.0695e+05      5.0461e+05       5.038e+05
v  Local Time Step            0.01         0.15558        0.010027        0.010171


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.8141       2.381e+06          258.45          13.425


 TIME FOR THE TIME STEP               28:        0.16253E+03

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


 INSTANT    0.290000000E+01   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        -0.289138223E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491793E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32810E+00 0.90154E+00
   Friction velocity        uet   :  0.90933E-02 0.17353E+02
   Friction velocity        uk    :  0.90856E-02 0.17353E+02
   Dimensionless distance   yplus :  0.17941E-02 0.69429E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        566
   Nb of faces within the viscous sub-layer     :      33756
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------   Friction velocity        uet   :  0.60491E-02 0.17540E+02
   Friction velocity        uk    :  0.60306E-02 0.17540E+02
   Dimensionless distance   yplus :  0.22381E-02 0.69485E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        569
   Nb of faces within the viscous sub-layer     :      33756
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24640E+00     343   0.12176E+00      Friction velocity        uet   :  0.60491E-02 0.17540E+02
   Friction velocity        uk    :  0.60306E-02 0.17540E+02
   Dimensionless distance   yplus :  0.22381E-02 0.69485E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        569
   Nb of faces within the viscous sub-layer     :      33756
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24640E+00     343   0.12176E+00   0.43395E-01 0.19915E+01 
c  Velocity[X]                                      0.10674E-01 
c  Velocity[Y]                                      0.17273E-01 
c  Velocity[Z]                                      0.15449E-01 
c  Pressure     0.12405E-01    1087   0.23975E-01   0.60199E-01 0.12312E+00 
c  k            0.72189E-02     157   0.25493E-03   0.50792E-05 0.24997E+01 
c  epsilon      0.20476E+02     100   0.31897E-03   0.38139E+02 0.63973E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.2827e-05                             8
a  epsilon               -0.042618                             9
a  Local Time Step      4.2278e-08                        280666


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.1755           2.201         0.22481        0.050145
v  Velocity[Y]             -2.2712          3.1187         0.14513         0.11937
v  Velocity[Z]             -3.9734          2.6087        -0.11656     -0.00038685
v  ǁVelocityǁ           0.00028854          4.3539         0.72239         0.98886
v  Pressure                -404.87          6933.4          4588.5            3788
v  k                    2.1527e-09         0.15519       0.0016077       0.0045816
v  epsilon              2.1528e-05            1030          2.2204          1.5438
v  TurbVisc             1.9228e-14         0.11253      0.00035839        0.004362
v  CourantNb             0.0075404           23278          41.366          10.677
v  FourierNb               0.22176      2.3653e+06          217.25          2.7515
v  total_pressure        4.996e+05      5.0693e+05      5.0459e+05      5.0379e+05
v  Local Time Step            0.01         0.17324        0.010027        0.010175


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.8355      2.3814e+06          258.62          13.429


 TIME FOR THE TIME STEP   Friction velocity        uet   :  0.60491E-02 0.17540E+02
   Friction velocity        uk    :  0.60306E-02 0.17540E+02
   Dimensionless distance   yplus :  0.22381E-02 0.69485E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        569
   Nb of faces within the viscous sub-layer     :      33756
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24640E+00     343   0.12176E+00   0.43395E-01 0.19915E+01 
c  Velocity[X]                                      0.10674E-01 
c  Velocity[Y]                                      0.17273E-01 
c  Velocity[Z]                                      0.15449E-01 
c  Pressure     0.12405E-01    1087   0.23975E-01   0.60199E-01 0.12312E+00 
c  k            0.72189E-02     157   0.25493E-03   0.50792E-05 0.24997E+01 
c  epsilon      0.20476E+02     100   0.31897E-03   0.38139E+02 0.63973E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.2827e-05                             8
a  epsilon               -0.042618                             9
a  Local Time Step      4.2278e-08                        280666


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.1755           2.201         0.22481        0.050145
v  Velocity[Y]             -2.2712          3.1187         0.14513         0.11937
v  Velocity[Z]             -3.9734          2.6087        -0.11656     -0.00038685
v  ǁVelocityǁ           0.00028854          4.3539         0.72239         0.98886
v  Pressure                -404.87          6933.4          4588.5            3788
v  k                    2.1527e-09         0.15519       0.0016077       0.0045816
v  epsilon              2.1528e-05            1030          2.2204          1.5438
v  TurbVisc             1.9228e-14         0.11253      0.00035839        0.004362
v  CourantNb             0.0075404           23278          41.366          10.677
v  FourierNb               0.22176      2.3653e+06          217.25          2.7515
v  total_pressure        4.996e+05      5.0693e+05      5.0459e+05      5.0379e+05
v  Local Time Step            0.01         0.17324        0.010027        0.010175


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.8355      2.3814e+06          258.62          13.429


 TIME FOR THE TIME STEP               30:        0.16099E+03

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


 INSTANT    0.310000000E+01   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       TIME FOR THE TIME STEP               31:        0.16111E+03

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


 INSTANT    0.320000000E+01   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        -0.863130573E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491796E+0 TIME FOR THE TIME STEP               31:        0.15824E+03

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


 INSTANT    0.320000000E+01   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        -0.863130573E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491796E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.33967E+00 0.89385E+00
   Friction velocity        uet   :  0.52260E-02 0.17078E+02
   Friction velocity        uk    :  0.52103E-02 0.17078E+02
   Dimensionless distance   yplus :  0.13318E-02 0.69817E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        569
   Nb of faces within the viscous sub-layer     :      33734
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24638E+00     338   0.11904E+00   0.39385E-01 0.18968E+01 
c  Velocity[X]                                      0.10513E-01 
c  Velocity[Y]                                      0.13978E-01 
c  Velocity[Z]                                      0.14894E-01 
c  Pressure     0.11999E-01    1010   0.22779E-01   0.58362E-01 0.74728E-01 
c  k            0.72278E-02     176   0.29940E-03   0.77253E-05 0.30822E+01 
c  epsilon      0.20564E+02      89   0.31015E-03   0.57007E+02 0.77983E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.6894e-05                             9
a  epsilon               -0.041807                            11
a  Local Time Step      4.2278e-08                        280684


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

   fiel TIME FOR THE TIME STEP               31:        0.16528E+03

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


 INSTANT    0.320000000E+01   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        -0.863130573E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491796E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.33967E+00 0.89385E+00
   Friction velocity        uet   :  0.52260E-02 0.17078E+02
   Friction velocity        uk    :  0.52103E-02 0.17078E+02
   Dimensionless distance   yplus :  0.13318E-02 0.69817E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        569
   Nb of faces within the viscous sub-layer     :      33734
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24638E+00     338   0.11904E+00   0.39385E-01 0.18968E+01 
c  Velocity[X]                                      0.10513E-01 
c  Velocity[Y]                                      0.13978E-01 
c  Velocity[Z]                                      0.14894E-01 
c  Pressure     0.11999E-01    1010   0.22779E-01   0.58362E-01 0.74728E-01 
c  k            0.72278E-02     176   0.29940E-03   0.77253E-05 0.30822E+01 
c  epsilon      0.20564E+02      89   0.31015E-03   0.57007E+02 0.77983E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.6894e-05                             9
a  epsilon               -0.041807                            11
a  Local Time Step      4.2278e-08                        280684


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.1633          2.2226         0.22451        0.050227
v  Velocity[Y]             -2.2865          3.1946         0.14563         0.11932
v  Velocity[Z]             -3.9012           2.607        -0.11809     -0.00033778
v  ǁVelocityǁ            0.0005146          4.2735         0.72505         0.98883
v  Pressure                -414.14          6920.3          4575.9          3781.2
v  k                    2.0919e-09         0.15
   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.1441          2.2091         0.22411         0.05028
v  Velocity[Y]             -2.2851          2.9978         0.14584         0.11934
v  Velocity[Z]              -3.925          2.6115        -0.11849     -0.00028923
v  ǁVelocityǁ           0.00040914           4.299         0.72577         0.98866
v  Pressure                -415.25          6915.5            4571          3778.4
v  k                    2.1522e-09         0.15491       0.0016132       0.0045836
v  epsilon              6.8649e-06          1024.6          2.2503          1.5523
v  TurbVisc             1.9821e-14         0.11253      0.00035303       0.0043601
v  Cour
   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.1441          2.2091         0.22411         0.05028
v  Velocity[Y]             -2.2851          2.9978         0.14584         0.11934
v  Velocity[Z]              -3.925          2.6115        -0.11849     -0.00028923
v  ǁVelocityǁ           0.00040914           4.299         0.72577         0.98866
v  Pressure                -415.25          6915.5            4571          3778.4
v  k                    2.1522e-09         0.15491       0.0016132       0.0045836
v  epsilon              6.8649e-06          1024.6          2.2503          1.5523
v  TurbVisc             1.9821e-14         0.11253      0.00035303       0.0043601
v  CourantNb             0.0030178           22632           41.57          10.681
v  FourierNb               0.22182      2.3653e+06          217.25          2.7502
v  total_pressure       4.9958e+05      5.0692e+05      5.0457e+05      5.0378e+05
v  Local Time Step            0.01         0.17323        0.010025        0.010169


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.8243      2.3845e+06          258.82          13.431


 TIME FOR THE TIME STEP               33:        0.15840E+03

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


 INSTANT    0.340000000E+01   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        -0.197735535E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491791E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37291E+00 0.89793E+00
   Friction velocity        uet   :  0.90170E-02 0.16716E+02
   Friction velocity        uk    :  0.89883E-02 0.16716E+02
   Dimensionless distance   yplus :  0.15789E-02 0.70952E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        569
   Nb of faces within the viscous sub-layer     :      33729
   Total number of wall face
   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.1441          2.2091         0.22411         0.05028
v  Velocity[Y]             -2.2851          2.9978         0.14584         0.11934
v  Velocity[Z]              -3.925          2.6115        -0.11849     -0.00028923
v  ǁVelocityǁ           0.00040914           4.299         0.72577         0.98866
v  Pressure                -415.25          6915.5            4571          3778.4
v  k                    2.1522e-09         0.15491       0.0016132       0.0045836
v  epsilon              6.8649e-06          1024.6          2.2503          1.5523
v  TurbVisc             1.9821e-14         0.11253      0.00035303       0.0043601
v  CourantNb             0.0030178           22632           41.57          10.681
v  FourierNb               0.22182      2.3653e+06          217.25          2.7502
v  total_pressure       4.9958e+05      5.0692e+05      5.0457e+05      5.0378e+05
v  Local Time Step            0.01         0.17323        0.010025        0.010169


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.8243      2.3845e+06          258.82          13.431


 TIME FOR THE TIME STEP               33:        0.15714E+03

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


 INSTANT    0.340000000E+01   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        -0.197735535E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491791E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37291E+00 0.89793E+00
   Friction velocity        uet   :  0.90170E-02 0.16716E+02
   Friction velocity        uk    :  0.89883E-02 0.16716E+02
   Dimensionless distance   yplus :  0.15789E-02 0.70952E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        569
   Nb of faces within the viscous sub-layer     :      33729
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24633E+00     328   0.11711E+00   0.38101E-01 0.18655E+01 
c  Velocity[X]                                      0.99432E-02 
c  Velocity[Y]                                      0.14010E-01    Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24634E+00     322   0.11773E+00   0.36369E-01 0.18230E+01 
c  Velocity[X]                                      0.98374E-02 
c  Velocity[Y]                                      0.12751E-01 
c  Velocity[Z]                                      0.13780E-01 
c  Pressure     0.11627E-01    1063   0.21416E-01   0.56810E-01 0.11209E+00 
c  k            0.72308E-02     177   0.30341E-03   0.37101E-05 0.   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24634E+00     322   0.11773E+00   0.36369E-01 0.18230E+01 
c  Velocity[X]                                      0.98374E-02 
c  Velocity[Y]                                      0.12751E-01 
c  Velocity[Z]                                      0.13780E-01 
c  Pressure     0.11627E-01    1063   0.21416E-01   0.56810E-01 0.11209E+00 
c  k            0.72308E-02     177   0.30341E-03   0.37101E-05 0.21365E+01 
c  epsilon      0.20664E+02      93   0.29164E-03   0.43290E+02 0.67709E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.9639e-05                            11
a  epsilon               -0.041346                            13
a  Local Time Step      4.2278e-08                        280751


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.1365          2.2216         0.22346        0.050349
v  Velocity[Y]             -2.2933          3.1216         0.14633         0.11945
v  Velocity[Z]             -3.7969          2.6181        -0.11857     -0.00023572
v  ǁVelocityǁ           0.00039341          4.1701         0.72724         0.98847
v  Pressure                -419.96          6905.8          4561.4          3772.1
v  k                     2.369e-09         0.15494       0.0016112       0.0045785
v  epsilon              9.9419e-06          1024.3          2.2428          1.5496
v  TurbVisc             2.2794e-14         0.11253       0.0003487       0.0043586
v  CourantNb            0.00095948           22800          41.596          10.679
v  FourierNb               0.22183      2.3653e+06          217.24          2.7491
v  total_pressure       4.9958e+05      5.0691e+05      5.0456e+05      5.0377e+05
v  Local Time Step            0.01         0.17322        0.010024        0.010161


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.8328      2.3863e+06          258.84          13.429


 TIME FOR THE TIME STEP               35:        0.15824E+03

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


 INSTANT    0.360000000E+01   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        -0.171246373E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491794E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40024E+00 0.89321E+00
   Friction velocity        uet   :  0.12161E-01 0.16328E+02
   Friction velocity        uk    :  0.12135E-01 0.16328E+02
   Dimensionless distance   yplus :  0.19057E-02 0.71846E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        575
   Nb of faces within the viscous sub-layer     :      33732
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24633E+00     323   0.11808E+00   0.35215E-01 0.17939E+01 
c  Velocity[X]                                      0.93511E-02 
c  Velocity[Y]                                      0.12307E-01 
c  Velocity[Z]                                      0.13556E-01 
c  Pressure     0.11558E-01     990   0.21479E-01   0.56564E-01 0.74744E-01 
c  k            0.72278E-02     173   0.32292E-03   0.67443E-05 0.28810E+01 
c  epsilon      0.20616E+02      89   0.43824E-03   0.89613E+02 0.97532E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.2054e-05                            10
a  epsilon               -0.034913                            12
a  Local Time Step      4.2278e-08                        280770


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.1274          2.2204         0.22289        0.050368
v  Velocity[Y]             -2.3048           3.288         0.14653         0.11951
v  Velocity[Z]             -3.9043          2.6221        -0.11861     -0.00022111
v  ǁVelocityǁ           0.00035756          4.2662         0.72757         0.98831
v  Pressure                -419.34          6902.5            4557          3769.5
v  k                    2.1705e-09         0.15349       0.0016106       0.0045766
v  epsilon              2.3465e-05          1006.2          2.2412          1.5486
v  TurbVisc              2.147e-14         0.11253      0.00034669        0.004358
v  CourantNb             0.0022452           22104          41.618          10.679
v  FourierNb               0.22182      2.3653e+06       ---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.167952533E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491794E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUN---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.167952533E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491794E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42429E+00 0.89108E+00
   Friction velocity        uet   :  0.90593E-02 0.15630E+02
   Friction velocity        uk    :  0.90552E-02 0.15630E+02
   Dimensionless distance   yplus :  0.18998E-02 0.72617E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        578
   Nb of faces within the viscous sub-layer     :      33734
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
 ---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.167952533E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491794E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42429E+00 0.89108E+00
   Friction velocity        uet   :  0.90593E-02 0.15630E+02
   Friction velocity        uk    :  0.90552E-02 0.15630E+02
   Dimensionless distance   yplus :  0.18998E-02 0.72617E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        578
   Nb of faces within the viscous sub-layer     :      33734
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24628E+00     314   0.12020E+00   0.35221E-01 0.17946E+01 
c  Velocity[X]                                      0.89134E-02 
c  Velocity[Y]                                      0.12692E-01 
c  Velocity[Z]                                      0.13615E-01 
c  Pressure     0.11392E-01    1065   0.21022E-01   0.55840E-01 0.11859E+00 
c  k            0.72237E-02     171   0.24543E-03   0.60956E-05 0.27400E+01 
c  epsilon      0.20594E+02      98   0.28504E-03   0.48528E+02 0.71961E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.8855e-05                            12
a  epsilon               -0.044751                            13
a  Local Time Step      4.2278e-08                        280771


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.1059          2.2191         0.22257        0.050392
v  Velocity[Y]             -2.3028          3.1548         0.14685         0.11957
v  Velocity[Z]             -3.7701          2.6153        -0.11858     -0.00016895
v  ǁVelocityǁ           0.00028474          4.1047         0.72787         0.98802
v  Pressure                -421.86          6894.8            4550          3764.9
v  k                    2.2163e-09         0.15526       0.0016081       0.0045734
v  epsilon              2.3634e-05          1025.1           2.237          1.5455
v  TurbVisc             1.9108e-14         0.11253      0.00034482       0.0043571
v  CourantNb             0.0020318           22625            41.6          10.677
v  FourierNb               0.22181      2.3653e+06          217.24          2.7483
v  total_pressure       4.9958e+05      5.0689e+05      5.0455e+05      5.0376e+05
v  Local Time Step            0.01         0.17321        0.010024        0.010156


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.8111      2.3871e+06          258.84          13.425


 TIME FOR THE TIME STEP               37:        0.16785E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.964733769E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491801E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   v  Velocity[Z]             -3.8459          2.6317        -0.11856        -0.00017
v  ǁVelocityǁ           0.00013508          4.2134          0.7281         0.98784
v  Pressure                -419.92            6891          4545.6          3762.3
v  k                    2.2795e-09         0.15502       0.0016035         0.00457
v  epsilon              2.3448e-05          1021.7          2.2298           1.542
v  TurbVisc              2.085e-14         0.11253      0.00034303       0.0043565
v  CourantNb              0.012479           22769          41.603          10.674
v  FourierNb               0.22179      2.3653e+06          217.23          2.7485
v  total_pressure       4.9958e+05      5.0689e+05      5.0455e+05      5.0376e+05
v  Local Time Step            0.01         0.17321        0.010023        0.010155


  ** Cv  Velocity[Z]             -3.8459          2.6317        -0.11856        -0.00017
v  ǁVelocityǁ           0.00013508          4.2134          0.7281         0.98784
v  Pressure                -419.92            6891          4545.6          3762.3
v  k                    2.2795e-09         0.15502       0.0016035         0.00457
v  epsilon              2.3448e-05          1021.7          2.2298           1.542
v  TurbVisc              2.085e-14         0.11253      0.00034303       0.0043565
v  CourantNb              0.012479           22769          41.603          10.674
v  FourierNb               0.22179      2.3653e+06          217.23          2.7485
v  total_pressure       4.9958e+05      5.0689e+05      5.0455e+05      5.0376e+05
v  Local Time Step            0.01         0.17321        0.010023        0.010155


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.8008      2.3881e+06          258.84          13.422


 TIME FOR THE TIME STEP               38:        0.15726E+03

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


 INSTANT    0.390000000E+01   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        -0.106010777E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491802E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44561E+00 0.88895E+00
   Friction velocity        uet   :  0.11874E-01 0.14838E+02
   Friction velocity        uk    :  0.11871E-01 0.14838E+02
   Dimensionless distance   yplus :  0.18720E-02 0.73264E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        574
   Nb of faces within the viscous sub-layer     :      33753
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24621E+00     320   0.11555E+00   0.34171E-01 0.17681E+01 
c  Velocity[X]                                      0.90062E-02 
c  Velocity[Y]                                      0.11836E-01 
c  Velocity[Z]                                      0.13329E-01 
c  Pressure     0.11072E-01    1047   0.20237E-01   0.54371E-01 0.12024E+00 
c  k            0.72126E-02     157   0.23885E-03   0.59901E-05 0.27181E+01 
c  epsilon      0.20539E+02      93   0.35963E-03   0.46473E+02 0.70600E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.1272e-05                            10
a  epsilon               -0.042813                            10
a  Local Time Step      4.2278e-08                        280788


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.1036          2.2214         0.22198        0.050373
v  Velocity[Y]             -2.3006          3.1009         0.14699         0.11967
v  Velocity[Z]             -3.8275           2.635        -0.11833     -0.00018342
v  ǁVelocityǁ           8.1042e-05          4.1746         0.72815         0.98767
v  Pressure                -422.55            6884          4538.8          3757.9
v  k                    2.2654e-09         0.15397       0.0016023       0.0045666
v  epsilon              2.3198e-05          1010.9          2.2335          1.5387
v  TurbVisc             2.0989e-14         0.11253      0.00034163       0.0043558
v  CourantNb            0.00032551           23350          41.602          10.672
v  FourierNb               0.22177      2.3653e+06          217.23          2.7476
v  total_pressure       4.9958e+05      5.0688e+05      5.0454e+05      5.0376e+05
v  Local Time Step            0.01         0.17321        0.010023        0.010153


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7892      2.3886e+06          258.83          13.419


 TIME FOR THE TIME STEP               39:        0.15551E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.131929773E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491786E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     -----------------------------------------------------------------------------
c  Velocity     0.24608E+00     315   0.11586E+00   0.33683E-01 0.17555E+01 
c  Velocity[X]                                      0.87355E-02 
c  Velocity[Y]                                      0.11365E-01 
c  Velocity[Z]                                      0.13582E-01 
c  Pressure     0.10860E-01    1140   0.19714E-01   0.53310E-01 0.12306E+00 
c  k            0.72089E-02     162   0.31587E-03   0.78531E-05 0.31122E+01 
c  epsilon      0.20522E+02     104   0.40238E-03   0.69816E+02 0.86413E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  ---------------------------------------------------------------------------------
c  Velocity     0.24608E+00     315   0.11586E+00   0.33683E-01 0.17555E+01 
c  Velocity[X]                                      0.87355E-02 
c  Velocity[Y]                                      0.11365E-01 
c  Velocity[Z]                                      0.13582E-01 
c  Pressure     0.10860E-01    1140   0.19714E-01   0.53310E-01 0.12306E+00 
c  k            0.72089E-02     162   0.31587E-03   0.78531E-05 0.31122E+01 
c  epsilon      0.20522E+02     104   0.40238E-03   0.69816E+02 0.86413E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.3636e-06                             7
a  epsilon               -0.031874                             8
a  Local Time Step      4.2278e-08                        280797


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0933          2.2224          0.2217         0.05037
v  Velocity[Y]             -2.3156          3.3017         0.14692         0.11973
v  Velocity[Z]             -3.8903           2.635         -0.1181     -0.00018706
v  ǁVelocityǁ           3.8465e-05          4.2396         0.72805         0.98746
v  Pressure                -4-----------------------------------------------------------------------------
c  Velocity     0.24608E+00     315   0.11586E+00   0.33683E-01 0.17555E+01 
c  Velocity[X]                                      0.87355E-02 
c  Velocity[Y]                                      0.11365E-01 
c  Velocity[Z]                                      0.13582E-01 
c  Pressure     0.10860E-01    1140   0.19714E-01   0.53310E-01 0.12306E+00 
c  k            0.72089E-02     162   0.31587E-03   0.78531E-05 0.31122E+01 
c  epsilon      0.20522E+02     104   0.40238E-03   0.69816E+02 0.86413E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.3636e-06                             7
a  epsilon               -0.031874                             8
a  Local Time Step      4.2278e-08                        280797


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0933          2.2224          0.2217         0.05037
v  Velocity[Y]             -2.3156          3.3017         0.14692         0.11973
v  Velocity[Z]             -3.8903           2.635         -0.1181     -0.00018706
v  ǁVelocityǁ           3.8465e-05          4.2396         0.72805         0.98746
v  Pressure                -422.97          6876.5          4531.8          3753.4
v  k                    2.4214e-09         0.15307        0.001606       0.0045661
v  epsilon              2.2854e-05          999.58           2.238          1.5397
v  TurbVisc             2.0817e-14         0.11253      0.00034037       0.0043553
v  CourantNb             0.0056011           22590          41.568          10.669
v  FourierNb               0.22174      2.3653e+06          217.23           2.747
v  total_pressure       4.9958e+05      5.0688e+05      5.0453e+05      5.0375e+05
v  Local Time Step            0.01          0.1732        0.010023        0.010149


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7871      2.3879e+06           258.8          13.416


 TIME FOR THE TIME STEP               40:        0.16277E+03

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


 INSTANT    0.410000000E+01   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        -0.134075281E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491807E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.47648E+00 0.89117E+00
   Friction velocity        uet   :  0.67003E-02 0.13915E+02
   Friction velocity        uk    :  0.67001E-02 0.13915E+02
   Dimensionless distance   yplus :  0.17298E-02 0.74210E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        567
   Nb of faces within the viscous sub-layer     :      33769
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24603E+00     319   0.11807E+00   0.33820E-01 0.17598E+01 
c  Velocity[X]                                      0.83555E-02 
c  Velocity[Y]                                      0.12178E-01 
c  Velocity[Z]                                      0.13287E-01 
c  Pressure     0.10741E-01    1118   0.19142E-01   0.52763E-01 0.97765E-01 
c  k            0.72007E-02     154   0.24986E-03   0.72186E-05 0.29860E+01 
c  epsilon      0.20469E+02      94   0.26178E-03   0.69097E+02 0.86413E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ----Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491795E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43973E+00 0.88722E+00
   Friction velocity        uet   :  0.49341E-02 0.13855E+02Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491795E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43973E+00 0.88722E+00
   Friction velocity        uet   :  0.49341E-02 0.13855E+02
   Friction velocity        uk    :  0.49333E-02 0.13855E+02
   Dimensionless distance   yplus :  0.16753E-02 0.73077E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        568
   Nb of faces within the viscous sub-layer     :      33767
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24599E+00     308   0.11779E+00   0.32062E-01 0.17136E+01 
c  Velocity[X]                                      0.82620E-02 
c  Velocity[Y]                                      0.10939E-01 
c  Velocity[Z]                                      0.12860E-01 
c  Pressure     0.10237E-01    1007   0.18141E-01   0.50358E-01 0.79170E-01 
c  k            0.71970E-02     147   0.27289E-03   0.50150E-05 0.24886E+01 
c  epsilon      0.20433E+02      94   0.35407E-03   0.45678E+02 0.70165E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.1177e-05                             9
a  epsilon               -0.039456                            10
a  Local Time Step      4.2278e-08                        280816


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -1.078          2.2184         0.22138        0.050368
v  Velocity[Y]             -2.3174          3.2743         0.14707         0.11979
v  Velocity[Z]             -3.9013          2.6439        -0.11797     -0.00023209
v  ǁVelocityǁ           3.7776e-05          4.2566         0.72828         0.98707
v  Pressure                -422.87            6867          4521.8          3747.8
v  k                    2.1976e-09          0.1553       0.0015993       0.0045622
v  epsilon              2.2497e-05          1023.6          2.2306          1.5333
v  TurbVisc             2.1914e-14         0.11253      0.00033804       0.0043547
v  CourantNb             0.0082191           22078          41.518          10.664
v  FourierNb               0.22168      2.3653e+06          217.23           2.747
v  total_pressure       4.9958e+05      5.0687e+05      5.0452e+05      5.0375e+05
v  Local Time Step            0.01          0.1732        0.010023        0.010147


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7792      2.3863e+06          258.75          13.411


 TIME FOR THE TIME STEP               42:        0.14977E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.376170420E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491781E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.48330E+00 0.88750E+00
   Friction velocity        uet   :  0.59565E-02 0.13078E+02
   Friction velocity        uk    :  0.59564E-02 0.13078E+02
   Dimensionless distance   yplus :  0.16687E-02 0.74427E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        569
   Nb of faces within the viscous sub-layer     :      33780
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24583E+00     318   0.11529E+00   0.32007E-01 0.17125E+01 
c  Velocity[X]                                      0.80731E-02 
c  Velocity[Y]                                      0.10814E-01 
c  Velocity[Z]                                      0.13119E-01 
c  Pressure     0.10277E-01    1064   0.17860E-01   0.50613E-01 0.12216E+00 
c  k            0.71941E-02     148   0.24931E-03   0.54698E-05 0.26000E+01 
c  epsilon      0.20453E+02      97   0.27794E-03   0.49237E+02 0.72980E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00027956                            15
a  epsilon         v  epsilon              1.1996e-06          1016.1          2.2121          1.5293
v  TurbVisc             1.8904e-14         0.11253       0.0003378       0.0043544
v  CourantNb             0.0042349           22914           41.53          10.662
v  FourierNb               0.22165      2.3653e+06          217.23          2.7468
v  total_pressure       4.9958e+05      5.0686e+05      5.0451e+05      5.0374e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010146


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7724      2.3882e+06          258.76          13.408


 TIME FOR THE TIME STEP     v  epsilon              1.1996e-06          1016.1          2.2121          1.5293
v  TurbVisc             1.8904e-14         0.11253       0.0003378       0.0043544
v  CourantNb             0.0042349           22914           41.53          10.662
v  FourierNb               0.22165      2.3653e+06          217.23          2.7468
v  total_pressure       4.9958e+05      5.0686e+05      5.0451e+05      5.0374e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010146


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7724      2.3882e+06          258.76          13.408


 TIME FOR THE TIME STEP               43:        0.15847E+03

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


 INSTANT    0.440000000E+01   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        -0.185706762E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491793E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46176E+00 0.88888E+00
   Friction velocity        uet   :  0.24699E-02 0.13212E+02
   Friction velocity        uk    :  0.24697E-02 0.13212E+02
   Dimensionless distance   yplus :  0.14543E-02 0.73780E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        570
   Nb of faces within the viscous sub-layer     :      33783
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24577E+00     310   0.11480E+00   0.30699E-01 0.16773E+01 
c  Velocity[X]                                      0.78212E-02 
c  Velocity[Y]                                      0.10728E-01 
c  Velocity[Z]                                      0.12150E-01v  epsilon              1.1996e-06          1016.1          2.2121          1.5293
v  TurbVisc             1.8904e-14         0.11253       0.0003378       0.0043544
v  CourantNb             0.0042349           22914           41.53          10.662
v  FourierNb               0.22165      2.3653e+06          217.23          2.7468
v  total_pressure       4.9958e+05      5.0686e+05      5.0451e+05      5.0374e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010146


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7724      2.3882e+06          258.76          13.408


 TIME FOR THE TIME STEP               43:        0.15186E+03

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


 INSTANT    0.440000000E+01   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        -0.185706762E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491793E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46176E+00 0.88888E+00
   Friction velocity        uet   :  0.24699E-02 0.13212E+02
   Friction velocity        uk    :  0.24697E-02 0.13212E+02
   Dimensionless distance   yplus :  0.14543E-02 0.73780E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        570
   Nb of faces within the viscous sub-layer     :      33783
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24577E+00     310   0.11480E+00   0.30699E-01 0.16773E+01 
c  Velocity[X]                                      0.78212E-02 
c  Velocity[Y]                                      0.10728E-01 
c  Velocity[Z]                                      0.12150E-01 
c  Pressure     0.97489E-02     986   0.16704E-01   0.48037E-01 0.58246E-01 
c  k            0.71916E-02     137   0.26081E-03   0.45383E-05 0.23685E+01 
c  epsilon      0.20451E+02      86   0.26172E-03   0.38934E+02 0.64843E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                 c  Velocity[Z]                                      0.12329E-01 
c  Pressure     0.95598E-02     838   0.16024E-01   0.47114E-01 0.47538E-01 
c  k            0.71875E-02     154   0.26137E-03   0.54141E-05 0.25878E+01 
c  epsilon      0.20432E+02      99   0.34925E-03   0.48312E+02 0.72351E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00026129                            16
a  epsilon                -0.40573                            13
a  Local Time Step      4.2278e-08                        280824


  ** Computed fields on cells
   c  Velocity[Z]                                      0.12329E-01 
c  Pressure     0.95598E-02     838   0.16024E-01   0.47114E-01 0.47538E-01 
c  k            0.71875E-02     154   0.26137E-03   0.54141E-05 0.25878E+01 
c  epsilon      0.20432E+02      99   0.34925E-03   0.48312E+02 0.72351E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00026129                            16
a  epsilon                -0.40573                            13
a  Local Time Step      4.2278e-08                        280824


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0712          2.2204         0.22134        0.050304
v  Velocity[Y]             -2.2964          3.1573         0.14747         0.11982
v  Velocity[Z]             -3.7761          2.6446        -0.11784     -0.00026402
v  ǁVelocityǁ           0.00011838          4.1201         0.72867         0.98668
v  Pressure                 -421.6          6855.1            4509          3739.8
v  k                    2.3164e-09         0.15575       0.0015883       0.0045551
v  epsilon              2.1109e-05          1028.4          2.2155          1.5256
v  TurbVisc             2.3107e-14         0.11253      0.00033607       0.0043538
v  CourantNb            5.4645e-05           22309          41.514          10.659
v  FourierNb               0.22159      2.3653e+06          217.23           2.746
v  total_pressure       4.9958e+05      5.0686e+05      5.0451e+05      5.0374e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010145


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7633      2.3876e+06          258.74          13.405


 TIME FOR THE TIME STEP               45:        0.14176E+03

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


 INSTANT    0.460000000E+01   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        -0.173550960E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491797E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         c  Velocity[Z]                                      0.12329E-01 
c  Pressure     0.95598E-02     838   0.16024E-01   0.47114E-01 0.47538E-01 
c  k            0.71875E-02     154   0.26137E-03   0.54141E-05 0.25878E+01 
c  epsilon      0.20432E+02      99   0.34925E-03   0.48312E+02 0.72351E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00026129                            16
a  epsilon                -0.40573                            13
a  Local Time Step      4.2278e-08                        280824


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0712          2.2204         0.22134        0.050304
v  Velocity[Y]             -2.2964          3.1573         0.14747         0.11982
v  Velocity[Z]             -3.7761          2.6446        -0.11784     -0.00026402
v  ǁVelocityǁ           0.00011838          4.1201         0.72867         0.98668
v  Pressure                 -421.6          6855.1            4509          3739.8
v  k                    2.3164e-09         0.15575       0.0015883       0.0045551
v  epsilon              2.1109e-05          1028.4          2.2155          1.5256
v  TurbVisc             2.3107e-14         0.11253      0.00033607       0.0043538
v  CourantNb            5.4645e-05           22309          41.514          10.659
v  FourierNb               0.22159      2.3653e+06          217.23           2.746
v  total_pressure       4.9958e+05      5.0686e+05      5.0451e+05      5.0374e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010145


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7633      2.3876e+06          258.74          13.405


 TIME FOR THE TIME STEP               45:        0.14123E+03

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


 INSTANT    0.460000000E+01   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        -0.173550960E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491797E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.45873E+00 0.88738E+00
   Friction velocity        uet   :  0.54140E-02 0.12319E+02
   Friction velocity        uk    :  0.54136E-Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.47825E+00 0.88752E+00
   Friction velocity        uet   :  0.44048E-02 0.11749E+02
   Friction velocity        uk    :  0.44046E-02 0.11749E+02
   Dimensionless distance   yplus :  0.14991E-02 0.74308E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        569
   Nb of facesFree surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.47825E+00 0.88752E+00
   Friction velocity        uet   :  0.44048E-02 0.11749E+02
   Friction velocity        uk    :  0.44046E-02 0.11749E+02
   Dimensionless distance   yplus :  0.14991E-02 0.74308E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        569
   Nb of faces within the viscous sub-layer     :      33796
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24567E+00     316   0.11498E+00   0.29521E-01 0.16451E+01 
c  Velocity[X]                                      0.76013E-02 
c  Velocity[Y]                                      0.10366E-01 
c  Velocity[Z]                                      0.11554E-01 
c  Pressure     0.93210E-02    1009   0.15282E-01   0.46015E-01 0.69610E-01 
c  k            0.71864E-02     148   0.23068E-03   0.61420E-05 0.27563E+01 
c  epsilon      0.20420E+02      96   0.26933E-03   0.74767E+02 0.89996E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00025683                            15
a  epsilon                -0.40219                            14
a  Local Time Step      4.2278e-08                        280827


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0686          2.2227         0.22142        0.050273
v  Velocity[Y]             -2.3005          3.1852         0.14742         0.11985
v  Velocity[Z]             -3.7987          2.6476         -0.1178     -0.00028487
v  ǁVelocityǁ           0.00016413          4.1566         0.72889         0.98656
v  Pressure                 -423.2            6849          4503.2          3736.4
v  k                    2.4909e-09         0.15412       0.0015835       0.0045541
v  epsilon              1.1269e-05          1011.9          2.2052          1.5246
v  TurbVisc             2.2229e-14         0.11253      0.00033493       0.0043531
v  CourantNb             0.0091056           22544           41.55          10.658
v  FourierNb               0.22154      2.3653e+06          217.23          2.7461
v  total_pressure       4.9958e+05      5.0685e+05       5.045e+05      5.0374e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010145


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7605      2.3878e+06          258.78          13.404


 TIME FOR THE TIME STEP               47:        0.15197E+03

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


 INSTANT    0.480000000E+01   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         0.202698862E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491783E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43318E+00 0.88457E+00
   Friction velocity        uet   :  0.63388E-02 0.11693E+02
   Friction velocity        uk    :  0.63384E-02 0.11693E+02
   Dimensionless distance   yplus :  0.14921E-02 0.72922E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        572
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24555E+00     299   0.11370E+00   0.29699E-01 0.16499E+01 
c  Velocity[X]                                      0.74047E-02 
c  Velocity[Y]                                      0.10559E-01 
c  Velocity[Z]                                      0.11735E-01 
c  Pressure     0.93044E-02     961   0.14926E-01   0.45956E-01 0.53767E-01 
c  k            0.71826E-02     144   0.21195E-03   0.37112E-05 0.21425E+01 
c  epsilon      0.20369E+02      93   0.33793E-03   0.35889E+02 0.62395E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.2654e-05                             9
a  epsilon               -0.041645                            12
a  Local Time Step      4.2278e-08                        280837


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

   field                   minimum         maximum        set mean    spativ  FourierNb               0.22152      2.3653e+06          217.22          2.7467
v  total_pressure       4.9958e+05      5.0685e+05       5.045e+05      5.0373e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010146


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7601      2.3879e+06          258.78          13.404


 TIME FOR THE TIME STEP               48:        0.15137E+03

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


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




   ** BOUNDARY MASv  FourierNb               0.22152      2.3653e+06          217.22          2.7467
v  total_pressure       4.9958e+05      5.0685e+05       5.045e+05      5.0373e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010146


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7601      2.3879e+06          258.78          13.404


 TIME FOR THE TIME STEP               48:        0.14287E+03

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


 INSTANT    0.490000000E+01   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         0.190854041E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491796E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.45268E+00 0.88716E+00
   Friction velocity        uet   :  0.62915E-02 0.10978E+02
   Friction velocity        uk    :  0.62764E-02 0.10978E+02
   Dimensionless distance   yplus :  0.14008E-02 0.73544E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        571
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24560E+00     313   0.11548E+00   0.29059E-01 0.16321E+01 
c  Velocity[X]                                      0.75110E-02 
c  Velocity[Y]                                      0.10054E-01 
c  Velocity[Z]                                      0.11494E-01 
c  Pressure     0.91505E-02     899   0.14424E-01   0.45250E-01 0.45518E-01 
c  k            0.71872E-02     143   0.21254E-03   0.28025E-05 0.18616E+01 
c  epsilon      0.20418E+02      98   0.22659E-03   0.26338E+02 0.53397E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.2032e-05                            10
a  epsilon               -0.089081                            13
a  Local Time Step      4.2278e-08                        280830


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0656          2.2322         0.22139        0.050225
v  Velocity[Y]             -2.3039          3.1085         0.14748         0.11991
v  Velocity[Z]              -3.868           2.644        -0.11795     -0.00029465
v  ǁVelocityǁ           0.00010234          4.2137         0.72928         0.98649
v  Pressure                -424.21          6843.2          4497.6          3732.9
v  k                    2.3611e-09         0.15566       0.0015877       0.0045545
v  epsilon              1.7449e-05          1024.9          2.2138          1.5255
v  TurbVisc              1.977e-14         0.11253      0.00033413       0.0043528
v  CourantNb              0.001455           22191          41.564          10.658
v  FourierNb                0.2215      2.3653e+06          217.22          2.7461
v  total_pressure       4.9958e+05      5.0684e+05       5.045e+05      5.0373e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010147


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7606      2.3875e+06          258.79          13.404


 TIME FOR THE TIME STEP               49:        0.15733E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.458034579E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491787E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.47174E+00 0.88860E+00
   Friction velocity        uet   :  0.68228E-02 0.11262E+02
   Friction velocity        uk    :  0.68065E-02 0.11262E+02
   Dimensionless distance   yplus :  0.14370E-02 0.74137E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        572
   Nb of faces within the viscous sub-layer     :      33795
   Total number of wall faces                   :      41000
--------------------------------------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -4.354e-05                            10
a  epsilon               -0.044217                            11
a  Local Time Step      4.2278e-08                        280829


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0639          2.2318         0.22148        0.050209
v  Velocity[Y]     -----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -4.354e-05                            10
a  epsilon               -0.044217                            11
a  Local Time Step      4.2278e-08                        280829


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0639          2.2318         0.22148        0.050209
v  Velocity[Y]             -2.3197          3.2359         0.14751         0.11994
v  Velocity[Z]             -3.8256          2.6473        -0.11798     -0.00030188
v  ǁVelocityǁ           5.5293e-05          4.1845         0.72949         0.98656
v  Pressure                -423.13          6841.6          4496.1          3732.3
v  k                    2.5179e-09         0.15476       0.0015853       0.0045545
v  epsilon              1.7785e-05          1017.5          2.2096          1.5254
v  TurbVisc             2.2275e-14         0.11253      0.00033398       0.0043527
v  CourantNb             0.0073141           23348          41.569          10.658
v  FourierNb               0.22149      2.3653e+06          217.22          2.7462
v  total_pressure       4.9958e+05      5.0684e+05       5.045e+05      5.0373e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010148


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7572      2.3886e+06          258.79          13.404


 TIME FOR THE TIME STEP               50:        0.13795E+03

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


 INSTANT    0.510000000E+01   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        -0.219218482E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491788E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42885E+00 0.88669E+00
   Friction velocity        uet   :  0.64479E-02 0.10644E+02
   Friction velocity        uk    :  0.64478E-02 0.10644E+02
   Dimensionless distance   yplus :  0.13582E-02 0.72803E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        571
   Nb of faces within the viscous sub-layer     :      33796
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24560E+00     309   0.11549E+00   0.28982E-01 0.16298E+01 
c  Velocity[X]                                      0.73935E-02 
c  Velocity[Y]                                      0.96064E-02 
c  Velocity[Z]                                      0.11982E-01 
c  Pressure     0.90460E-02     903   0.14316E-01   0.44758E-01 0.63090E-01 
c  k            0.71840E-02     150   0.19993E-03   0.34721E-05 0.20721E+01 
c  epsilon      0.20396E+02      98   0.26182E-03   0.45756E+02 0.70444E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.1563e-05                            11
a  epsilon               -0.069408                            10
a  Local Time Step      4.2278e-08                        280818


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0692          2.2327         0.22151         0.05017
v  Velocity[Y]             -2.2965          3.0943         0.14756         0.11994
v  Velocity[Z]             -3.8893          2.6508        -0.11805     -0.00030472
v  ǁVelocityǁ            3.457e-05          4.2466         0.72955         0.98654
v  Pressure                -426.46          6837.8          4492.5          3729.8
v  k                    2.2676e-09         0.15399       0.0015859       0.0045539
v  epsilon              1.7429e-05          1010.7          2.2088          1.5246
v  TurbVisc             2.2868e-14         0.11253      0.00033366       0.0043526
v  CourantNb              0.023052           24024          41.591          10.659
v  FourierNb               0.22148      2.3653e+06          217.22          2.7466
v  total_pressure       4.9957e+05      5.0684e+05      5.0449e+05      5.0373e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010146


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7584      2.3893e+06          258.81          13.406


 TIME FOR THE TIME STEP               51:        0.15027E+03

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


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




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

---------------------------------------------------------------
Boundary typ------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44174E+00 0.88686E+00
   Friction velocity        uet   :  0.65686E-02 0.10234E+02
   Friction velocity        uk    :  0.65605E-02 0.10234E+02
   Dimensionless distance   yplus :  0.13058E-02 0.73225E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        577
   Nb of faces within the viscous sub-layer     :      33790
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
------------------------------------------------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44174E+00 0.88686E+00
   Friction velocity        uet   :  0.65686E-02 0.10234E+02
   Friction velocity        uk    :  0.65605E-02 0.10234E+02
   Dimensionless distance   yplus :  0.13058E-02 0.73225E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        577
   Nb of faces within the viscous sub-layer     :      33790
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24558E+00     299   0.11319E+00   0.28950E-01 0.16288E+01 
c  Velocity[X]                                      0.73457E-02 
c  Velocity[Y]                                      0.97560E-02 
c  Velocity[Z]                                      0.11849E-01 
c  Pressure     0.88375E-02     907   0.13915E-01   0.43723E-01 0.43976E-01 
c  k            0.71851E-02     154   0.21898E-03   0.40943E-05 0.22498E+01 
c  epsilon      0.20402E+02     101   0.34125E-03   0.31409E+02 0.58286E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.7425e-05                            10
a  epsilon               -0.055315                            13
a  Local Time Step      4.2278e-08                        280830


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0665           2.238         0.22146        0.050174
v  Velocity[Y]             -2.3141          3.2136         0.14755         0.11995
v  Velocity[Z]             -3.8094          2.6388        -0.11819     -0.00029143
v  ǁVelocityǁ           0.00013718          4.1693         0.72966         0.98651
v  Pressure                -424.57          6835.5            4490          3728.3
v  k                    2.3091e-09         0.15496       0.0015904       0.0045546
v  epsilon               1.715e-05          1019.9          2.2219          1.5264
v  TurbVisc             1.9302e-14         0.11253      0.00033351       0.0043525
v  CourantNb             0.0043204           22779          41.586          10.659
v  FourierNb               0.22148      2.3653e+06          217.22          2.7459
v  total_pressure       4.9958e+05      5.0684e+05      5.0449e+05      5.0373e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010144


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7579      2.3881e+06          258.81          13.405


 TIME FOR THE TIME STEP               52:        0.14463E+03

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


 INSTANT    0.530000000E+01   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        -0.165324729E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491791E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43717E+00 0.88653E+00
   Friction velocity        uet   :  0.53631E-02 0.95953E+01
   Friction velocity        uk    :  0.53628E-02 0.95953E+01
   Dimensionless distance   yplus :  0.12244E-02 0.73090E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        573
   Nb of faces within the viscous sub-layer     :      33795
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24562E+00     299   0.11404E+00   0.27683E-01 0.15928E+01 
c  Velocity[X]                                      0.74589E-02 
c  Velocity[Y]                                      0.93681E-02 
c  Velocity[Z]                                      0.10856E-01 
c  Pressure     0.87927E-02     888   0.13810E-01   0.43525E-01 0.53141E-01 
c  k            0.71870E-02     138   0.18903E-03   0.30679E-05 0.19477E+01 
c  epsilon      0.20446E+02      88   0.21421E-03   0.24546E+02 0.51527E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.7978e-05                            10
a  epsilon               -0.059033                            10
a  Local Time Step      4.2278e-08                        280824


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0678          2.2415         0.22147        0.050143
v  Velocity[Y]             -2.2986          2.9239         0.14761         0.11995
v  Velocity[Z]             -3.8499          2.6344    
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7593      2.3882e+06          258.82          13.405


 TIME FOR THE TIME STEP               53:        0.14984E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Sm
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7593      2.3882e+06          258.82          13.405


 TIME FOR THE TIME STEP               53:        0.14663E+03

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


 INSTANT    0.540000000E+01   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         0.199572061E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491794E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42608E+00 0.88724E+00
   Friction velocity        uet   :  0.97743E-02 0.95113E+01
   Friction velocity        uk    :  0.97732E-02 0.95113E+01
   Dimensionless distance   yplus :  0.12136E-02 0.72752E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        576
   Nb of faces within the viscous sub-layer     :      33785
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24557E+00     300   0.11406E+00   0.28791E-01 0.16244E+01 
c  Velocity[X]                                      0.77657E-02 
c  Velocity[Y]                                      0.99518E-02 
c  Velocity[Z]                                      0.11074E-01 
c  Pressure     0.89370E-02     890   0.13981E-01   0.44259E-01 0.30821E-01 
c  k            0.71830E-02     126   0.20473E-03   0.43088E-05 0.23080E+01 
c  epsilon      0.20390E+02      84   0.29448E-03   0.53952E+02 0.76344E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.8294e-05                            10
a  epsilon                -0.06269                            14
a  Local Time Step      4.2278e-08                        280821


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0714          2.2333         0.22156        0.050098
v  Velocity[Y]             -2.3091          3.2144         0.14762         0.11997
v  Velocity[Z]             -3.8122          2.6296        -0.11842     -0.00028296
v  ǁVelocityǁ           0.00014506          4.1726         0.72991         0.98648
v  Pressure                -423.95          6831.3          4485.9          3725.4
v  k                    2.3266e-09         0.15497       0.0015863       0.0045544
v  epsilon              1.6501e-05          1021.3          2.2113          1.5254
v  TurbVisc             2.2559e-14         0.11253      0.00033314       0.0043522
v  CourantNb              0.010986           23785           41.62           10.66
v  FourierNb               0.22146      2.3653e+06          217.22          2.7457
v  total_pressure       4.9958e+05      5.0683e+05      5.0449e+05      5.0373e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010144


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7628      2.3891e+06          258.84          13.405


 TIME FOR THE TIME STEP               54:        0.13938E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.361540750E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491798E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43042E+00 0.88688E+00
   Friction velocity        uet   :  0.99301E-02 0.87623E+01
   Friction velocity        uk    :  0.99093E-02 0.87623E+01
   Dimensionless distance   yplus :  0.11181E-02 0.72900E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        577
   Nb of faces within the viscous sub-layer     :      33796
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-------------------------------------------------------a  k                   -4.5075e-05                            10
a  epsilon               -0.055127                            12
a  Local Time Step      4.2278e-08                        280829


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0623          2.2371         0.22153        0.050072
v  Velocity[Y]             -2.2999          3.0459         0.14779         0.11999
v  Velocity[Z]             -3.9065          2.6412        -0.11825      -0.0002872
v  ǁVelocityǁ           0.00012073          4.2678         0.72996         0.98644
v  Pressure                -423.01          6829.1            4484          3723.9a  k                   -4.5075e-05                            10
a  epsilon               -0.055127                            12
a  Local Time Step      4.2278e-08                        280829


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0623          2.2371         0.22153        0.050072
v  Velocity[Y]             -2.2999          3.0459         0.14779         0.11999
v  Velocity[Z]             -3.9065          2.6412        -0.11825      -0.0002872
v  ǁVelocityǁ           0.00012073          4.2678         0.72996         0.98644
v  Pressure                -423.01          6829.1            4484          3723.9
v  k                    2.4037e-09         0.15447       0.0015879       0.0045534
v  epsilon              1.6153e-05          1015.9          2.2179          1.5255
v  TurbVisc             2.0204e-14         0.11253      0.00033312       0.0043522
v  CourantNb              0.013555           23282          41.619          10.659
v  FourierNb               0.22146      2.3653e+06          217.22           2.746
v  total_pressure       4.9958e+05      5.0683e+05      5.0448e+05      5.0372e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010145


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7658      2.3886e+06          258.84          13.405


 TIME FOR THE TIME STEP               55:        0.14859E+03

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


 INSTANT    0.560000000E+01   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        -0.280114043E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491784E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44015E+00 0.88696E+00
   Friction velocity        uet   :  0.79894E-02 0.92495E+01
   Friction velocity        uk    :  0.79876E-02 0.92495E+01
   Dimensionless distance   yplus :  0.11802E-02 0.73207E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        576
   Nb of faces within the viscous sub-layer     :      33789
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24560E+00     289   0.11400E+00   0.28234E-01 0.16084E+01 
c  Velocity[X]                                      0.71917E-02 
c  Velocity[Y]                                      0.98435E-02 
c  Velocity[Z]                                      0.11199E-01 
c  Pressure     0.90259E-02     899   0.14010E-01   0.44713E-01 0.32083E-01 
c  k            0.71865E-02     149   0.22914E-03   0.33471E-05 0.20345E+01 
c  epsilon      0.20433E+02      96   0.37706E-03   0.38700E+02 0.64701E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.3714e-05                            10
a  epsilon                -0.12119                            13
a  Local Time Step      4.2278e-08                        280817


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0616          2.2343         0.22163        0.050081
v  Velocity[Y]              -2.298          3.1781         0.14769         0.11997
v  Velocity[Z]             -3.9041          2.6343         -0.1184     -0.00028218
v  ǁVelocityǁ           0.00015499          4.2542         0.72996         0.98647
v  Pressure                -423.06          6827.4          4482.5            3723
v  k                    2.5169e-09         0.15536       0.0015873       0.0045531
v  epsilon              1.5867e-05          1024.1          2.2167          1.5249
v  TurbVisc             2.2588e-14         0.11253       0.0003331       0.0043521
v  CourantNb             0.0040903           24299          41.628           10.66
v  FourierNb               0.22146      2.3653e+06          217.22          2.7454
v  total_pressure       4.9958e+05      5.0683e+05      5.0448e+05      5.0372e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010141


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7625      2.3896e+06          258.85          13.405


 TIME FOR THE TIME STEP               56:        0.14469E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.138659606E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+0   Dimensionless distance   yplus :  0.99879E-03 0.71824E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        575
   Nb of faces within the viscous sub-layer     :      33797
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24561E+00     299   0.11470E+00   0.28031E-01 0.16025E+01 
c  Velocity[X]                                      0.74301E-02 
c  Velocity[Y]                     Dimensionless distance   yplus :  0.99879E-03 0.71824E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        575
   Nb of faces within the viscous sub-layer     :      33797
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24561E+00     299   0.11470E+00   0.28031E-01 0.16025E+01 
c  Velocity[X]                                      0.74301E-02 
c  Velocity[Y]                                      0.92401E-02 
c  Velocity[Z]                                      0.11360E-01 
c  Pressure     0.92226E-02     937   0.14194E-01   0.45659E-01 0.48016E-01 
c  k            0.71866E-02     128   0.17409E-03   0.28213E-05 0.18681E+01 
c  epsilon      0.20430E+02      88   0.17964E-03   0.19867E+02 0.46440E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.4209e-05                            10
a  epsilon               -0.064066                            10
a  Local Time Step      4.2278e-08                        280832


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0619          2.2354         0.22151        0.050059
v  Velocity[Y]             -2.2927          3.0273         0.14794            0.12
v  Velocity[Z]             -3.7804          2.6342        -0.11848     -0.00028219
v  ǁVelocityǁ           0.00024372           4.137         0.72997         0.98651
v  Pressure                -426.04          6824.2            4480          3721.2
v  k                    2.3349e-09         0.15418       0.0015826        0.004552
v  epsilon              1.5606e-05          1013.2           2.203          1.5227
v  TurbVisc             2.2452e-14         0.11253      0.00033281       0.0043519
v  CourantNb             0.0024509           24153          41.614           10.66
v  FourierNb               0.22145      2.3653e+06          217.22           2.746
v  total_pressure       4.9957e+05      5.0682e+05      5.0448e+05      5.0372e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010142


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7654      2.3894e+06          258.84          13.406


 TIME FOR THE TIME STEP               57:        0.14565E+03

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


 INSTANT    0.580000000E+01   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        -0.168383782E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491787E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42940E+00 0.88653E+00
   Friction velocity        uet   :  0.91298E-02 0.77022E+01
   Friction velocity        uk    :  0.91182E-02 0.77022E+01
   Dimensionless distance   yplus :  0.98280E-03 0.72894E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        581
   Nb of faces within the viscous sub-layer     :      33790
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24561E+00     287   0.11446E+00   0.28718E-01 0.16220E+01 
c  Velocity[X]                                      0.77930E-02 
c  Velocity[Y]                                      0.96711E-02 
c  Velocity[Z]                                      0.11254E-01 
c  Pressure     0.90699E-02     612   0.13778E-01   0.44896E-01 0.16440E-01 
c  k            0.71864E-02     124   0.24698E-03   0.38902E-05 0.21931E+01 
c  epsilon      0.20441E+02      84   0.32535E-03   0.50604E+02 0.73836E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.5637e-05                            10
a  epsilon               -0.056398                            13
a  Local Time Step      4.2278e-08                        280837


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0676          2.2392          0.2217        0.050085
v  Velocity[Y]             -2.2973           3.151         0.14808         0.12003
v  Velocity[Z]             -3.9283          2.6328        -0.11868     -0.00029091
v  ǁVelocityǁ           0.00022094          4.2789         0.73031         0.98652
v  Pressure                -425.61          6823.9          4479.8            3721
v  k                    2.3612e-09         0.15546        0.001586        0.004553
v  epsilon               1.537e-05          1025.1          2.2112          1.5253
v  TurbVisc       INSTANT    0.590000000E+01   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         0.173840515E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491792E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+0 INSTANT    0.590000000E+01   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         0.173840515E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491792E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38440E+00 0.88574E+00
   Friction velocity        uet   :  0.63124E-02 0.71475E+01
   Friction velocity        uk    :  0.63047E-02 0.71475E+01
   Dimensionless distance   yplus :  0.91202E-03 0.71413E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        575
   Nb of faces within the viscous sub-layer     :      33795
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24569E+00     298   0.11630E+00   0.27867E-01 0.15977E+01 
c  Velocity[X]                                      0.71278E-02 
c  Velocity[Y]                                      0.93822E-02 
c  Velocity[Z]                                      0.11357E-01 
c  Pressure     0.86126E-02     798   0.13045E-01   0.42616E-01 0.35052E-01 
c  k            0.71850E-02     150   0.20088E-03   0.37426E-05 0.21516E+01 
c  epsilon      0.20438E+02      98   0.28291E-03   0.46565E+02 0.71031E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.3128e-05                            10
a  epsilon               -0.062597                            11
a  Local Time Step      4.2278e-08                        280827


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0646          2.2353         0.22158        0.050084
v  Velocity[Y]             -2.2951          3.0045         0.14804         0.12005
v  Velocity[Z]             -3.7903          2.6337         -0.1186     -0.00028558
v  ǁVelocityǁ           0.00019755          4.1526         0.73037         0.98656
v  Pressure                -427.53          6822.5          4478.1          3719.8
v  k                    2.4478e-09         0.15493       0.0015834       0.0045516
v  epsilon              1.5148e-05          1020.4          2.2047          1.5232
v  TurbVisc             2.1536e-14         0.11253      0.00033269       0.0043517
v  CourantNb             0.0060739           23283           41.63          10.662
v  FourierNb               0.22145      2.3653e+06          217.22          2.7457
v  total_pressure       4.9957e+05      5.0682e+05      5.0448e+05      5.0372e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010141


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7638      2.3886e+06          258.85          13.408


 TIME FOR THE TIME STEP               59:        0.14708E+03

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


 INSTANT    0.600000000E+01   TIME STEP NUMBER              60
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.285459691E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491785E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41812E+00 0.88639E+00
   Friction velocity        uet   :  0.78498E-02 0.76539E+01
   Friction velocity        uk    :  0.78445E-02 0.76539E+01
   Dimensionless distance   yplus :  0.97664E-03 0.72552E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        582
   Nb of faces within the viscous sub-layer     :      33784
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24564E+00     285   0.11247E+00   0.27863E-01 0.15975E+01 
c  Velocity[X]                                      0.71742E-02 
c  Velocity[Y]                                      0.94909E-02 
c  Velocity[Z]                                      0.11198E-01 
c  Pressure     0.87125E-02     636   0.13139E-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0582           2.239         0.22167        0.050105
v  Velocity[Y]             -2.3036          3.1586         0.14793         0.12008
v  Velocity[Z]             -3.8843          2.6298        -0.11873     -0.00028526
v  ǁVelocityǁ           0.00013792          4.2424         0.73055         0.98653
v  Pressure                -427.04          6821.9          4477.9          3719.5
v  k                    2.4358e-09         0.15487       0.0015904       0.0045528
v  epsilon              1.4969e-05          1020.4          2.2237          1.5255
v  TurbVisc             2.2228e-14         0.11253      0.00033251       0.0043516
v  CourantNb            0.00080234           23988          41.648          10.662
v  Fouri-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0582           2.239         0.22167        0.050105
v  Velocity[Y]             -2.3036          3.1586         0.14793         0.12008
v  Velocity[Z]             -3.8843          2.6298        -0.11873     -0.00028526
v  ǁVelocityǁ           0.00013792          4.2424         0.73055         0.98653
v  Pressure                -427.04          6821.9          4477.9          3719.5
v  k                    2.4358e-09         0.15487       0.0015904       0.0045528
v  epsilon              1.4969e-05          1020.4          2.2237          1.5255
v  TurbVisc             2.2228e-14         0.11253      0.00033251       0.0043516
v  CourantNb            0.00080234           23988          41.648          10.662
v  FourierNb               0.22144      2.3653e+06          217.22          2.7456
v  total_pressure       4.9957e+05      5.0682e+05      5.0448e+05      5.0372e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010141


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7642      2.3893e+06          258.87          13.408


 TIME FOR THE TIME STEP               60:        0.16536E+03

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


 INSTANT    0.610000000E+01   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         0.781641859E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491795E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37318E+00 0.88405E+00
   Friction velocity        uet   :  0.70641E-02 0.67715E+01
   Friction velocity        uk    :  0.70632E-02 0.67715E+01
   Dimensionless distance   yplus :  0.86405E-03 0.71054E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        583
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24564E+00     296   0.11214E+00   0.27141E-01 0.15767E+01 
c  Velocity[X]                                      0.72483E-02 
c  Velocity[Y]                                      0.89776E-02 
c  Velocity[Z]                                      0.10915E-01 
c  Pressure     0.84162E-02     819   0.12708E-01   0.41646E-01 0.30931E-01 
c  k            0.71873E-02     140   0.23329E-03   0.39088E-05 0.21988E+01 
c  epsilon      0.20421E+02      98   0.30212E-03   0.44706E+02 0.69599E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00025696                            13
a  epsilon                -0.45879                            13
a  Local Time Step      4.2278e-08                        280840


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0626          2.2361         0.22166        0.050067
v  Velocity[Y]             -2.2933          2.9988         0.14798         0.12009
v  Velocity[Z]             -3.8077          2.6382         -0.1188     -0.00030144
v  ǁVelocityǁ            0.0001131          4.1639         0.73069         0.98655
v  Pressure                -428.68          6820.2          4476.7          3718.4
v  k                    2.5421e-09         0.15453       0.0015845        0.004551
v  epsilon              1.4813e-05            1016            2.21          1.5236
v  TurbVisc             2.1893e-14         0.11253      0.00033267       0.0043515
v  CourantNb             0.0030175           23538          41.666          10.662
v  FourierNb               0.22144      2.3653e+06          217.22          2.7458
v  total_pressure       4.9957e+05      5.0682e+05      5.0448e+05      5.0372e+05
v  Local Time Step            0.01         0.17319        0.010022         0.01014


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7682      2.3888e+06          258.89          13.408


 TIME FOR THE TIME STEP               61:        0.19506E+03

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


 INSTANT    0.620000000E+01   TIME STEP NUMBER              62
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.113664036E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491804E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0     ------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24579E+00     284   0.11465E+00   0.27060E-01 0.15741E+01 
c  Velocity[X]                                      0.74210E-02 
c  Velocity[Y]                                      0.89496E-02 
c  Velocity[Z]                                      0.10689E-01 
c  Pressure     0.83565E-02     956   0.12558E-01   0.41352E-01 0.39951E-01 
c  k            0.71824E-02     139   0.22836E-03   0.42897E-05 0.23036E+01 
c  epsilon      0.20410E+02      91   0.37533E-03 ------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24579E+00     284   0.11465E+00   0.27060E-01 0.15741E+01 
c  Velocity[X]                                      0.74210E-02 
c  Velocity[Y]                                      0.89496E-02 
c  Velocity[Z]                                      0.10689E-01 
c  Pressure     0.83565E-02     956   0.12558E-01   0.41352E-01 0.39951E-01 
c  k            0.71824E-02     139   0.22836E-03   0.42897E-05 0.23036E+01 
c  epsilon      0.20410E+02      91   0.37533E-03   0.58994E+02 0.79770E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.5565e-05                            10
a  epsilon               -0.045031                            13
a  Local Time Step      4.2278e-08                        280840


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0702          2.2322         0.22175         0.05007
v  Velocity[Y]             -2.3077          3.1615         0.14794          0.1201
v  Velocity[Z]             -3.9444          2.6305        -0.11888     -0.00028178
v  ǁVelocityǁ           0.00023901          4.2991         0.73088         0.98652
v  Pressure                -430.66          6817.9          4474.5          3716.9
v  k                    2.5871e-09          0.1559       0.0015856       0.0045505
v  epsilon              1.4682e-05          1029.2          2.2142          1.5235
v  TurbVisc             2.3745e-14         0.11253       0.0003322       0.0043512
v  CourantNb            0.00043726           22891          41.662          10.662
v  FourierNb               0.22143      2.3653e+06          217.22          2.7461
v  total_pressure       4.9957e+05      5.0682e+05      5.0447e+05      5.0372e+05
v  Local Time Step            0.01         0.17318        0.010023         0.01014


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7627      2.3882e+06          258.89          13.408


 TIME FOR THE TIME STEP               62:        0.19829E+03

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


 INSTANT    0.630000000E+01   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        -0.171817829E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491801E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36864E+00 0.88510E+00
   Friction velocity        uet   :  0.52146E-02 0.56509E+01
   Friction velocity        uk    :  0.52133E-02 0.56509E+01
   Dimensionless distance   yplus :  0.71231E-03 0.70641E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        578
   Nb of faces within the viscous sub-layer     :      33788
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24575E+00     291   0.11471E+00   0.27946E-01 0.15999E+01 
c  Velocity[X]                                      0.73461E-02 
c  Velocity[Y]                                      0.93349E-02 
c  Velocity[Z]                                      0.11265E-01 
c  Pressure     0.84183E-02     615   0.12530E-01   0.41649E-01 0.14293E-01 
c  k            0.71853E-02     153   0.30920E-03   0.54922E-05 0.26062E+01 
c  epsilon      0.20429E+02     100   0.34872E-03   0.66412E+02 0.84710E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.1313e-05                             8
a  epsilon               -0.036484                             7
a  Local Time Step      4.2278e-08                        280831


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0684          2.2323          0.2217        0.050072
v  Velocity[Y]             -2.3002          2.9829         0.14812          0.1201
v  Velocity[Z]             -3.8797           2.632        -0.11887     -0.00029332
v  ǁVelocityǁ           7.4132e-05          4.2273         0.73097         0.98649
v  Pressure                 -429.3          6817.4          4474.2          3716.7
v  k                    2.3023e-09         0.15455       0.0015883       0.0045512
v  epsilon              1.8986e-06          1017.5          2.2166          1.5253
v  TurbVisc             2.2784e-14         0.11253      0.00033221        0.004351
v  CourantNb            0.00021731           24980          41.697          10.663
v  FourierNb               0.22143      2.3653e+06          217.22           2.746
v  total_pressure       4.9957e+05    Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.140854519E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491787E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ----------------------------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.140854519E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491787E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39411E+00 0.88644E+00
   Friction velocity        uet   :  0.99566E-02 0.61891E+01
   Friction velocity        uk    :  0.99558E-02 0.61891E+01
   Dimensionless distance   yplus :  0.73869E-03 0.71801E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        580
   Nb of faces within the viscous sub-layer     :      33789
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24575E+00     291   0.11314E+00   0.27443E-01 0.15854E+01 
c  Velocity[X]                                      0.74186E-02 
c  Velocity[Y]                                      0.90367E-02 
c  Velocity[Z]                                      0.10988E-01 
c  Pressure     0.83675E-02     396   0.12402E-01   0.41388E-01 0.15449E-01 
c  k            0.71819E-02     153   0.25553E-03   0.45790E-05 0.23804E+01 
c  epsilon      0.20399E+02     100   0.35918E-03   0.40499E+02 0.66227E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00022922                            16
a  epsilon                 -0.4242                            15
a  Local Time Step      4.2278e-08                        280831


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0683          2.2347         0.22168        0.050095
v  Velocity[Y]              -2.304          3.1536         0.14799         0.12011
v  Velocity[Z]             -3.8594          2.6342        -0.11878      -0.0002843
v  ǁVelocityǁ           0.00018471          4.2135          0.7309         0.98648
v  Pressure                -428.09          6817.3          4474.1          3716.9
v  k                    2.3711e-09         0.15516       0.0015876       0.0045495
v  epsilon              1.4457e-05          1021.8          2.2199          1.5233
v  TurbVisc             1.9489e-14         0.11253      0.00033212       0.0043509
v  CourantNb              0.019131           22336          41.693          10.663
v  FourierNb               0.22142      2.3653e+06          217.22          2.7455
v  total_pressure       4.9957e+05      5.0682e+05      5.0447e+05      5.0372e+05
v  Local Time Step            0.01         0.17318        0.010023        0.010139


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.763      2.3876e+06          258.92          13.409


 TIME FOR THE TIME STEP               64:        0.16402E+03

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


 INSTANT    0.650000000E+01   TIME STEP NUMBER              65
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.139825813E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491694E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36880E+00 0.88551E+00
   Friction velocity        uet   :  0.12051E-01 0.56921E+01
   Friction velocity        uk    :  0.12036E-01 0.56921E+01
   Dimensionless distance   yplus :  0.66417E-03 0.70296E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        581
   Nb of faces within the viscous sub-layer     :      33798
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24573E+00     295   0.11464E+00   0.27388E-01 0.15839E+01 
c  Velocity[X]                                      0.71282E-02 
c  Velocity[Y]                                      0.98411E-02 
c  Velocity[Z]                                      0.10418E-01 
c  Pressure     0.83812E-02     899   0.12491E-01   0.41468E-01 0.40349E-01 
c  k            0.71836E-02     138   0.19193E-03   0.30486E-05 0.19424E+01 
c  epsilon      0.20410E+02      87   0.26552E-03   0.22740E+02 0.49660E+01 
----------------------------------------------------------------v  Velocity[Z]             -3.8805          2.6322        -0.11865     -0.00029009
v  ǁVelocityǁ           0.00018906          4.2391         0.73074         0.98646
v  Pressure                -429.31          6815.4          4472.2          3715.3
v  k                    2.5378e-09         0.15499       0.0015835       0.0045483
v  epsilon              1.4354e-05          1020.4          2.2103          1.5218
v  TurbVisc             2.2111e-14         0.11253      0.00033187       0.0043505
v  CourantNb            0.00045754           24390           41.68          10.663
v  FourierNb               0.22142      2.3653e+06          217.22          2.7454
v  total_pressure       4.9957e+05      5.0682e+05      5.0447e+05      5.0372e+05
v  Local Time Step            0.01         0.17319        0.010023         0.01014


  ** Cv  Velocity[Z]             -3.8805          2.6322        -0.11865     -0.00029009
v  ǁVelocityǁ           0.00018906          4.2391         0.73074         0.98646
v  Pressure                -429.31          6815.4          4472.2          3715.3
v  k                    2.5378e-09         0.15499       0.0015835       0.0045483
v  epsilon              1.4354e-05          1020.4          2.2103          1.5218
v  TurbVisc             2.2111e-14         0.11253      0.00033187       0.0043505
v  CourantNb            0.00045754           24390           41.68          10.663
v  FourierNb               0.22142      2.3653e+06          217.22          2.7454
v  total_pressure       4.9957e+05      5.0682e+05      5.0447e+05      5.0372e+05
v  Local Time Step            0.01         0.17319        0.010023         0.01014


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7651      2.3897e+06           258.9          13.408


 TIME FOR THE TIME STEP               65:        0.19558E+03

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


 INSTANT    0.660000000E+01   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        -0.135980197E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491783E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38246E+00 0.88727E+00
   Friction velocity        uet   :  0.86518E-02 0.57179E+01
   Friction velocity        uk    :  0.85950E-02 0.57179E+01
   Dimensionless distance   yplus :  0.67438E-03 0.71420E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        578
   Nb of faces within the viscous sub-layer     :      33786
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24585E+00     280   0.11668E+00   0.27542E-01 0.15882E+01 
c  Velocity[X]                                      0.73320E-02 
c  Velocity[Y]                                      0.96246E-02 
c  Velocity[Z]                                      0.10585E-01 
c  Pressure     0.84629E-02     807   0.12561E-01   0.41899E-01 0.17360E-01 
c  k            0.71835E-02     131   0.23558E-03   0.45796E-05 0.23803E+01 
c  epsilon      0.20421E+02      86   0.33571E-03   0.60924E+02 0.81055E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.1148e-05                             9
a  epsilon               -0.043593                             7
a  Local Time Step      4.2278e-08                        280831


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0671          2.2375         0.22174        0.050081
v  Velocity[Y]             -2.3002          3.1528         0.14786         0.12013
v  Velocity[Z]             -3.9293          2.6332        -0.11881     -0.00029406
v  ǁVelocityǁ           6.3923e-05          4.2693         0.73094         0.98649
v  Pressure                -429.08          6814.3          4471.2          3714.9
v  k                      2.36e-09         0.15549       0.0015845       0.0045496
v  epsilon              1.4242e-05          1024.5           2.211          1.5236
v  TurbVisc             2.2987e-14         0.11253      0.00033163       0.0043504
v  CourantNb             0.0025821           23463          41.651          10.663
v  FourierNb               0.22142      2.3653e+06          217.22          2.7456
v  total_pressure       4.9957e+05      5.0681e+05      5.0447e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010142


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7649      2.3887e+06          258.87          13.408


 TIME FOR THE TIME STEP               66:        0.18386E+03

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


 INSTANT    0.670000000E+01   TIME STEP NUMBER              67
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.311314688E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491786E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     -----------------------------------------------------------------------------
c  Velocity     0.24579E+00     280   0.11506E+00   0.27405E-01 0.15842E+01 
c  Velocity[X]                                      0.72624E-02 
c  Velocity[Y]                                      0.91419E-02 
c  Velocity[Z]                                      0.11000E-01 
c  Pressure     0.81408E-02     850   0.12186E-01   0.40305E-01 0.29108E-01 
c  k            0.71815E-02     142   0.19254E-03   0.40524E-05 0.22397E+01 
c  epsilon      0.20416E+02      97   0.28527E-03   0.54532E+02 0.76926E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  ---------------------------------------------------------------------------------
c  Velocity     0.24579E+00     280   0.11506E+00   0.27405E-01 0.15842E+01 
c  Velocity[X]                                      0.72624E-02 
c  Velocity[Y]                                      0.91419E-02 
c  Velocity[Z]                                      0.11000E-01 
c  Pressure     0.81408E-02     850   0.12186E-01   0.40305E-01 0.29108E-01 
c  k            0.71815E-02     142   0.19254E-03   0.40524E-05 0.22397E+01 
c  epsilon      0.20416E+02      97   0.28527E-03   0.54532E+02 0.76926E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00023857                            15
a  epsilon                -0.42895                            14
a  Local Time Step      4.2278e-08                        280825


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0668          2.2331         0.22164        0.050068
v  Velocity[Y]             -2.2886          2.9772         0.14802         0.12014
v  Velocity[Z]             -3.7978           2.632        -0.11872     -0.00028456
v  ǁVelocityǁ           4.7938e-05          4.1519         0.73099         0.98648
v  Pressure                -427.46            6813            4470          3713.8
v  k                     2.386e-09         0.15436       0.0015821       0.0045479
v  epsilon              1.4131e-05          1013.9          2.2067          1.5214
v  TurbVisc             2.0237e-14         0.11253      0.00033162       0.0043505
v  CourantNb             0.0015856           24124          41.676          10.663
v  FourierNb               0.22142      2.3653e+06          217.22          2.7451
v  total_pressure       4.9957e+05      5.0681e+05      5.0447e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010141


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7654      2.3894e+06           258.9          13.409


 TIME FOR THE TIME STEP               67:        0.19078E+03

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


 INSTANT    0.680000000E+01   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         0.210855951E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491799E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37265E+00 0.88573E+00
   Friction velocity        uet   :  0.80558E-02 0.54442E+01
   Friction velocity        uk    :  0.80392E-02 0.54442E+01
   Dimensionless distance   yplus :  0.60271E-03 0.70711E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        575
   Nb of faces within the viscous sub-layer     :      33795
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24581E+00     294   0.11290E+00   0.26832E-01 0.15677E+01 
c  Velocity[X]                                      0.71186E-02 
c  Velocity[Y]                                      0.92198E-02 
c  Velocity[Z]                                      0.10494E-01 
c  Pressure     0.83219E-02     649   0.12317E-01   0.41192E-01 0.16032E-01 
c  k            0.71824E-02     153   0.19838E-03   0.24654E-05 0.17470E+01 
c  epsilon      0.20404E+02      99   0.33547E-03   0.22144E+02 0.49021E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.4048e-05                            12
a  epsilon               -0.042705                            14
a  Local Time Step      4.2278e-08                        280826


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0642          2.2358         0.22172        0.050083
v  Velocity[Y]             -2.2996          3.1641         0.14784         0.12017
v  Velocity[Z]             -3.9605          2.6369        -0.11879     -0.00028176
v  ǁVelocityǁ           0.00010461          4.3098          0.7311         0.98642
v  Pressure                -426.07          6812.2          4469.8          3713.6
v  k                    2.5321e-09         0.15509       0.0015859       0.0045482
v  epsilon              1.4029e-05          1021.5          2.2158          1.5217
v  TurbVisc             2.2105e-14         0.11253      0.00033134       0.0043504
v  CourantNb             0.0041788           23904          41.682          10.663
v  FourierNb               0.22142      2.3653e+06          217.22          2.7455
v  total_pressure       4.9957e+05      5.0681e+05      5.0447e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010141


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  ------Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491795E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36574E+00 0.88500E+00
   Friction velocity        uet   :  0.51350E-02 0.48459E+01Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491795E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36574E+00 0.88500E+00
   Friction velocity        uet   :  0.51350E-02 0.48459E+01
   Friction velocity        uk    :  0.51339E-02 0.48459E+01
   Dimensionless distance   yplus :  0.55195E-03 0.69879E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        578
   Nb of faces within the viscous sub-layer     :      33794
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24582E+00     290   0.11526E+00   0.27676E-01 0.15922E+01 
c  Velocity[X]                                      0.75617E-02 
c  Velocity[Y]                                      0.94975E-02 
c  Velocity[Z]                                      0.10617E-01 
c  Pressure     0.85715E-02     391   0.12738E-01   0.42434E-01 0.14600E-01 
c  k            0.71848E-02     146   0.16914E-03   0.30002E-05 0.19271E+01 
c  epsilon      0.20428E+02      96   0.20771E-03   0.18230E+02 0.44472E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.1152e-05                            11
a  epsilon               -0.099328                            11
a  Local Time Step      4.2278e-08                        280829


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0728          2.2405         0.22174        0.050059
v  Velocity[Y]             -2.2943          2.9702         0.14803         0.12014
v  Velocity[Z]             -3.7967          2.6275        -0.11871     -0.00028014
v  ǁVelocityǁ           2.4307e-05          4.1488         0.73115         0.98643
v  Pressure                   -425          6812.1          4469.7          3713.7
v  k                    2.3375e-09         0.15456       0.0015838       0.0045477
v  epsilon              1.3929e-05          1017.5          2.2087          1.5215
v  TurbVisc             2.2632e-14         0.11253      0.00033151       0.0043504
v  CourantNb             0.0027508           25458          41.707          10.664
v  FourierNb               0.22141      2.3653e+06          217.22          2.7451
v  total_pressure       4.9957e+05      5.0681e+05      5.0447e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023         0.01014


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7635      2.3907e+06          258.93          13.409


 TIME FOR THE TIME STEP               69:        0.16560E+03

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


 INSTANT    0.700000000E+01   TIME STEP NUMBER              70
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.215718696E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491640E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37268E+00 0.88716E+00
   Friction velocity        uet   :  0.41716E-02 0.51138E+01
   Friction velocity        uk    :  0.41711E-02 0.51138E+01
   Dimensionless distance   yplus :  0.53926E-03 0.70611E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        577
   Nb of faces within the viscous sub-layer     :      33802
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24586E+00     283   0.11519E+00   0.28244E-01 0.16083E+01 
c  Velocity[X]                                      0.73231E-02 
c  Velocity[Y]                                      0.98399E-02 
c  Velocity[Z]                                      0.11081E-01 
c  Pressure     0.84483E-02     481   0.12610E-01   0.41835E-01 0.15430E-01 
c  k            0.71815E-02     144   0.23049E-03   0.41469E-05 0.22657E+01 
c  epsilon      0.20421E+02      97   0.28208E-03   0.48656E+02 0.72484E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.0588e-05                            12
a  epsilon         v  epsilon              1.3822e-05          1024.5          2.2102          1.5214
v  TurbVisc             2.0063e-14         0.11253      0.00033137       0.0043504
v  CourantNb               0.01201           23611          41.691          10.664
v  FourierNb                0.2214      2.3653e+06          217.22          2.7458
v  total_pressure       4.9958e+05      5.0681e+05      5.0447e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010141


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7605      2.3889e+06          258.91          13.409


 TIME FOR THE TIME STEP     v  epsilon              1.3822e-05          1024.5          2.2102          1.5214
v  TurbVisc             2.0063e-14         0.11253      0.00033137       0.0043504
v  CourantNb               0.01201           23611          41.691          10.664
v  FourierNb                0.2214      2.3653e+06          217.22          2.7458
v  total_pressure       4.9958e+05      5.0681e+05      5.0447e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010141


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7605      2.3889e+06          258.91          13.409


 TIME FOR THE TIME STEP               70:        0.17429E+03

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


 INSTANT    0.710000000E+01   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         0.591404517E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491639E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36545E+00 0.88490E+00
   Friction velocity        uet   :  0.50756E-02 0.50046E+01
   Friction velocity        uk    :  0.50753E-02 0.50046E+01
   Dimensionless distance   yplus :  0.58395E-03 0.69702E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        577
   Nb of faces within the viscous sub-layer     :      33807
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24582E+00     290   0.11489E+00   0.28299E-01 0.16098E+01 
c  Velocity[X]                                      0.75036E-02 
c  Velocity[Y]                                      0.96521E-02 
c  Velocity[Z]                                      0.11143E-01 
c  Pressure     0.86711E-02     708   0.12940E-01   0.42902E-01 0.17928E-01 
c  k            0.71825E-02     135   0.25740E-03   0.44407E-05 0.23449E+01 
c  epsilon      0.20446E+02      87   0.31707E-03   0.57961E+02 0.79190E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.8635e-05                            12
a  epsilon               -0.065488                            13
a  Local Time Step      4.2278e-08                        280820


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0729          2.2427          0.2216        0.050045
v  Velocity[Y]             -2.2917           2.969         0.14803         0.12012
v  Velocity[Z]             -3.8092          2.6341        -0.11863     -0.00026076
v  ǁVelocityǁ           6.4882e-05          4.1599         0.73117          0.9865
v  Pressure                 -420.3          6811.3          4469.3          3713.5
v  k                    2.5694e-09           0.155       0.0015819       0.0045457
v  epsilon              1.3716e-05          1019.4          2.2082          1.5205
v  TurbVisc             2.2171e-14         0.11253      0.00033139       0.0043502
v  CourantNb             0.0069139           24313          41.705          10.665
v  FourierNb                0.2214      2.3653e+06          217.22          2.7454
v  total_pressure       4.9958e+05      5.0681e+05      5.0447e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023         0.01014


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7625      2.3896e+06          258.93           13.41


 TIME FOR THE TIME STEP               71:        0.18055E+03

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


 INSTANT    0.720000000E+01   TIME STEP NUMBER              72
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.636640911E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491798E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37825E+00 0.88514E+00
   Friction velocity        uet   :  0.59870E-02 0.49622E+01
   Friction velocity        uk    :  0.59856E-02 0.49622E+01
   Dimensionless distance   yplusc  Velocity[Z]                                      0.10649E-01 
c  Pressure     0.85663E-02     777   0.12860E-01   0.42380E-01 0.21117E-01 
c  k            0.71833E-02     137   0.20474E-03   0.37678E-05 0.21594E+01 
c  epsilon      0.20428E+02      92   0.33032E-03   0.27146E+02 0.54193E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.7067e-05                            11
a  epsilon               -0.064023                            12
a  Local Time Step      4.2278e-08                        280817


  ** Computed fields on cells
   c  Velocity[Z]                                      0.10649E-01 
c  Pressure     0.85663E-02     777   0.12860E-01   0.42380E-01 0.21117E-01 
c  k            0.71833E-02     137   0.20474E-03   0.37678E-05 0.21594E+01 
c  epsilon      0.20428E+02      92   0.33032E-03   0.27146E+02 0.54193E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.7067e-05                            11
a  epsilon               -0.064023                            12
a  Local Time Step      4.2278e-08                        280817


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0701          2.2411         0.22157        0.050081
v  Velocity[Y]             -2.2987          3.1702         0.14808         0.12016
v  Velocity[Z]             -3.9592          2.6329        -0.11877     -0.00025803
v  ǁVelocityǁ            0.0001285          4.3157         0.73129          0.9865
v  Pressure                -417.98            6810          4468.4          3712.8
v  k                    2.3718e-09         0.15482       0.0015852       0.0045475
v  epsilon              6.0509e-06          1018.7          2.2168           1.522
v  TurbVisc              2.334e-14         0.11253      0.00033117       0.0043501
v  CourantNb              0.020482           23650           41.67          10.665
v  FourierNb               0.22139      2.3653e+06          217.22          2.7457
v  total_pressure       4.9958e+05      5.0681e+05      5.0447e+05      5.0371e+05
v  Local Time Step            0.01         0.17318        0.010023        0.010142


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7614      2.3889e+06          258.89          13.411


 TIME FOR THE TIME STEP               72:        0.18518E+03

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


 INSTANT    0.730000000E+01   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         0.133777228E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491787E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37531E+00 0.88469E+00
   Friction velocity        uet   :  0.61086E-02 0.48564E+01
   Friction velocity        uk    :  0.61083E-02 0.48564E+01
   Dimensionless distance   yplus :  0.49773E-03 0.69804E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        581
   Nb of faces within the viscous sub-layer     :      33798
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24586E+00     283   0.11391E+00   0.27331E-01 0.15821E+01 
c  Velocity[X]                                      0.73256E-02 
c  Velocity[Y]                                      0.92407E-02 
c  Velocity[Z]                                      0.10765E-01 
c  Pressure     0.84041E-02     698   0.12528E-01   0.41571E-01 0.18423E-01 
c  k            0.71838E-02     155   0.20486E-03   0.34491E-05 0.20664E+01 
c  epsilon      0.20447E+02     103   0.27999E-03   0.19720E+02 0.46192E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.8915e-05                            12
a  epsilon                -0.23877                            15
a  Local Time Step      4.2278e-08                        280814


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0751           2.244         0.22167        0.050086
v  Velocity[Y]             -2.2891          2.9626         0.14812         0.12015
v  Velocity[Z]              -3.874          2.6346        -0.11879     -0.00028772
v  ǁVelocityǁ           6.1357e-05          4.2124         0.73133         0.98651
v  Pressure                -416.26          6809.5          4467.9          3712.6
v  k                     2.397e-09          0.1546       0.0015857       0.0045464
v  epsilon                1.35e-05          1017.3          2.2147          1.5217
v  TurbVisc             2.0055e-14         0.18155      0.00033186       0.0043504
v  CourantNb            0.00040186           23761          41.695          10.666
v  FourierNb               0.22139      2.3653e+06          217.22          2.7459
v  total_pressure       4.9958e+05      5.0681e+05      5.0447e+05      5.0371e+05
v  Local Time Step            0.01         0.17318        0.010023        0.010141


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7591       2.389e+06          258.92          13.412


 TIME FOR THE TIME STEP               73:        0.18202E+03

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


 IFree surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37240E+00 0.88811E+00
   Friction velocity        uet   :  0.53978E-02 0.49366E+01
   Friction velocity        uk    :  0.53975E-02 0.49366E+01
   Dimensionless distance   yplus :  0.49900E-03 0.71114E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        575
   Nb of facesFree surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37240E+00 0.88811E+00
   Friction velocity        uet   :  0.53978E-02 0.49366E+01
   Friction velocity        uk    :  0.53975E-02 0.49366E+01
   Dimensionless distance   yplus :  0.49900E-03 0.71114E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        575
   Nb of faces within the viscous sub-layer     :      33800
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24580E+00     288   0.11363E+00   0.27281E-01 0.15805E+01 
c  Velocity[X]                                      0.72761E-02 
c  Velocity[Y]                                      0.89108E-02 
c  Velocity[Z]                                      0.11094E-01 
c  Pressure     0.85331E-02     888   0.12703E-01   0.42192E-01 0.25050E-01 
c  k            0.71882E-02     149   0.19970E-03   0.39525E-05 0.22116E+01 
c  epsilon      0.20493E+02      96   0.29708E-03   0.52283E+02 0.74981E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.8914e-05                            12
a  epsilon               -0.058553                            14
a  Local Time Step      4.2278e-08                        280815


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0761          2.2351         0.22178        0.050101
v  Velocity[Y]                -2.3          3.1817         0.14806         0.12015
v  Velocity[Z]             -3.8815          2.6279        -0.11891     -0.00027641
v  ǁVelocityǁ           7.8237e-05          4.2353          0.7316         0.98655
v  Pressure                 -417.5          6808.3          4466.6          3711.7
v  k                    2.5341e-09         0.15579       0.0015827       0.0045463
v  epsilon              1.3403e-05          1028.8          2.2105          1.5216
v  TurbVisc             2.2271e-14         0.11253      0.00033117       0.0043499
v  CourantNb            0.00015409           23336          41.687          10.666
v  FourierNb               0.22138      2.3653e+06          217.22          2.7454
v  total_pressure       4.9958e+05      5.0681e+05      5.0447e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010141


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.762      2.3886e+06          258.91          13.412


 TIME FOR THE TIME STEP               74:        0.16935E+03

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


 INSTANT    0.750000000E+01   TIME STEP NUMBER              75
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.971335521E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491801E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37560E+00 0.88457E+00
   Friction velocity        uet   :  0.10107E-01 0.47220E+01
   Friction velocity        uk    :  0.10107E-01 0.47220E+01
   Dimensionless distance   yplus :  0.38321E-03 0.69835E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        579
   Nb of faces within the viscous sub-layer     :      33800
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24584E+00     291   0.11270E+00   0.27497E-01 0.15868E+01 
c  Velocity[X]                                      0.72713E-02 
c  Velocity[Y]                                      0.95737E-02 
c  Velocity[Z]                                      0.10652E-01 
c  Pressure     0.85608E-02     775   0.12688E-01   0.42341E-01 0.22708E-01 
c  k            0.71881E-02     129   0.20978E-03   0.27577E-05 0.18477E+01 
c  epsilon      0.20482E+02      91   0.26012E-03   0.40808E+02 0.66429E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.9919e-05                            11
a  epsilon               -0.069572                            13
a  Local Time Step      4.2278e-08                        280811


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

   field                   minimum         maximum        set mean    spativ  FourierNb               0.22137      2.3653e+06          217.22          2.7454
v  total_pressure       4.9958e+05      5.0681e+05      5.0447e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010141


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7583      2.3889e+06          258.94          13.413


 TIME FOR THE TIME STEP               75:        0.15764E+03

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


 INSTANT    0.760000000E+01   TIME STEP NUMBER              76
 ============================================================= 




   ** BOUNDARY MASv  FourierNb               0.22137      2.3653e+06          217.22          2.7454
v  total_pressure       4.9958e+05      5.0681e+05      5.0447e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010141


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7583      2.3889e+06          258.94          13.413


 TIME FOR THE TIME STEP               75:        0.16014E+03

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


 INSTANT    0.760000000E+01   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         0.688872348E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491797E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37865E+00 0.88655E+00
   Friction velocity        uet   :  0.86622E-02 0.49355E+01
   Friction velocity        uk    :  0.86620E-02 0.49355E+01
   Dimensionless distance   yplus :  0.43109E-03 0.70930E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        575
   Nb of faces within the viscous sub-layer     :      33801
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24590E+00     283   0.11278E+00   0.27637E-01 0.15908E+01 
c  Velocity[X]                                      0.74071E-02 
c  Velocity[Y]                                      0.93411E-02 
c  Velocity[Z]                                      0.10888E-01 
c  Pressure     0.84275E-02     790   0.12577E-01   0.41669E-01 0.23597E-01 
c  k            0.71823E-02     149   0.19359E-03   0.29097E-05 0.18978E+01 
c  epsilon      0.20439E+02      99   0.34050E-03   0.26303E+02 0.53319E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.4946e-05                            11
a  epsilon                 -0.0491                            14
a  Local Time Step      4.2278e-08                        280826


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0705          2.2337         0.22169        0.050108
v  Velocity[Y]             -2.2928          3.1599          0.1482         0.12015
v  Velocity[Z]             -3.9565          2.6377        -0.11886     -0.00027479
v  ǁVelocityǁ           0.00010072          4.2993          0.7315         0.98659
v  Pressure                -420.11          6806.2          4464.9          3710.6
v  k                    2.3732e-09         0.15528        0.001585       0.0045458
v  epsilon              1.3263e-05            1023          2.2192          1.5212
v  TurbVisc             2.0206e-14         0.11253      0.00033088       0.0043499
v  CourantNb             0.0092379           22971          41.692          10.667
v  FourierNb               0.22136      2.3653e+06          217.22          2.7458
v  total_pressure       4.9958e+05      5.0681e+05      5.0446e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010141


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7628      2.3883e+06          258.91          13.413


 TIME FOR THE TIME STEP               76:        0.16086E+03

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


 INSTANT    0.770000000E+01   TIME STEP NUMBER              77
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.810954013E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491779E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37241E+00 0.88468E+00
   Friction velocity        uet   :  0.84510E-02 0.44616E+01
   Friction velocity        uk    :  0.84506E-02 0.44616E+01
   Dimensionless distance   yplus :  0.30717E-03 0.69512E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        580
   Nb of faces within the viscous sub-layer     :      33809
   Total number of wall faces                   :      41000
--------------------------------------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.5638e-05                            12
a  epsilon               -0.065108                            13
a  Local Time Step      4.2278e-08                        280823


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0746          2.2408         0.22176        0.050076
v  Velocity[Y]     -----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.5638e-05                            12
a  epsilon               -0.065108                            13
a  Local Time Step      4.2278e-08                        280823


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0746          2.2408         0.22176        0.050076
v  Velocity[Y]             -2.2936           2.952          0.1482         0.12013
v  Velocity[Z]             -3.8355          2.6301        -0.11884     -0.00025121
v  ǁVelocityǁ           0.00011925          4.1834         0.73155         0.98663
v  Pressure                -421.13          6805.6          4464.3          3710.1
v  k                     2.582e-09         0.15459       0.0015826       0.0045447
v  epsilon              1.3231e-05          1017.3          2.2133            1.52
v  TurbVisc             2.1737e-14         0.11253       0.0003308       0.0043498
v  CourantNb             0.0036362           23698          41.691          10.669
v  FourierNb               0.22135      2.3653e+06          217.22          2.7453
v  total_pressure       4.9958e+05      5.0681e+05      5.0446e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010141


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7585       2.389e+06          258.91          13.414


 TIME FOR THE TIME STEP               77:        0.15622E+03

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


 INSTANT    0.780000000E+01   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         0.143744949E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491792E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37783E+00 0.88784E+00
   Friction velocity        uet   :  0.10583E-01 0.47008E+01
   Friction velocity        uk    :  0.10583E-01 0.47008E+01
   Dimensionless distance   yplus :  0.37289E-03 0.70509E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        580
   Nb of faces within the viscous sub-layer     :      33808
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24592E+00     282   0.11359E+00   0.26760E-01 0.15653E+01 
c  Velocity[X]                                      0.71901E-02 
c  Velocity[Y]                                      0.88821E-02 
c  Velocity[Z]                                      0.10688E-01 
c  Pressure     0.82129E-02     851   0.12144E-01   0.40584E-01 0.25834E-01 
c  k            0.71890E-02     125   0.19816E-03   0.34081E-05 0.20537E+01 
c  epsilon      0.20498E+02      86   0.31211E-03   0.47621E+02 0.71551E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -4.746e-05                            11
a  epsilon               -0.066892                            14
a  Local Time Step      4.2278e-08                        280825


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0679          2.2423         0.22176        0.050109
v  Velocity[Y]             -2.3003          3.1691         0.14813         0.12014
v  Velocity[Z]             -3.9686          2.6351        -0.11905     -0.00023771
v  ǁVelocityǁ           3.8813e-05          4.3199         0.73172         0.98664
v  Pressure                -423.72            6804            4463          3709.2
v  k                    2.3986e-09         0.15579       0.0015826       0.0045454
v  epsilon              1.3206e-05          1028.3          2.2132          1.5212
v  TurbVisc             2.3366e-14         0.11253      0.00033069       0.0043497
v  CourantNb             0.0073813           23427          41.695          10.669
v  FourierNb               0.22135      2.3653e+06          217.22          2.7457
v  total_pressure       4.9958e+05       5.068e+05      5.0446e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023         0.01014


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7625      2.3887e+06          258.92          13.415


 TIME FOR THE TIME STEP               78:        0.14648E+03

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


 INSTANT    0.790000000E+01   TIME STEP NUMBER              79
 ============================================================= 




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

---------------------------------------------------------------
Boundary typ------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38071E+00 0.88511E+00
   Friction velocity        uet   :  0.85140E-02 0.42888E+01
   Friction velocity        uk    :  0.85032E-02 0.42888E+01
   Dimensionless distance   yplus :  0.43693E-03 0.69005E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        575
   Nb of faces within the viscous sub-layer     :      33810
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
------------------------------------------------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38071E+00 0.88511E+00
   Friction velocity        uet   :  0.85140E-02 0.42888E+01
   Friction velocity        uk    :  0.85032E-02 0.42888E+01
   Dimensionless distance   yplus :  0.43693E-03 0.69005E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        575
   Nb of faces within the viscous sub-layer     :      33810
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24598E+00     295   0.11511E+00   0.27181E-01 0.15775E+01 
c  Velocity[X]                                      0.72838E-02 
c  Velocity[Y]                                      0.91936E-02 
c  Velocity[Z]                                      0.10704E-01 
c  Pressure     0.84840E-02     845   0.12507E-01   0.41909E-01 0.22630E-01 
c  k            0.71871E-02     155   0.19911E-03   0.37735E-05 0.21617E+01 
c  epsilon      0.20501E+02     102   0.29156E-03   0.49086E+02 0.72835E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.6767e-05                            12
a  epsilon               -0.057965                            15
a  Local Time Step      4.2278e-08                        280829


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0722          2.2442         0.22181        0.050143
v  Velocity[Y]               -2.29          2.9605         0.14821         0.12018
v  Velocity[Z]             -3.9036          2.6346        -0.11897     -0.00025009
v  ǁVelocityǁ           9.1071e-05          4.2443         0.73174         0.98667
v  Pressure                -421.36          6804.7          4463.9            3710
v  k                    2.3613e-09         0.15405       0.0015829       0.0045442
v  epsilon              1.3185e-05          1011.7          2.2124          1.5198
v  TurbVisc             2.0183e-14         0.11253      0.00033071       0.0043497
v  CourantNb             0.0062383           24076          41.729           10.67
v  FourierNb               0.22134      2.3653e+06          217.22          2.7453
v  total_pressure       4.9958e+05       5.068e+05      5.0446e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010141


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7557      2.3894e+06          258.95          13.415


 TIME FOR THE TIME STEP               79:        0.15640E+03

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


 INSTANT    0.800000000E+01   TIME STEP NUMBER              80
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.252394847E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491621E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37478E+00 0.88623E+00
   Friction velocity        uet   :  0.68595E-02 0.36775E+01
   Friction velocity        uk    :  0.68593E-02 0.36775E+01
   Dimensionless distance   yplus :  0.31788E-03 0.69650E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        575
   Nb of faces within the viscous sub-layer     :      33810
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24598E+00     284   0.11417E+00   0.27190E-01 0.15777E+01 
c  Velocity[X]                                      0.69443E-02 
c  Velocity[Y]                                      0.91727E-02 
c  Velocity[Z]                                      0.11073E-01 
c  Pressure     0.84397E-02     759   0.12418E-01   0.41739E-01 0.18552E-01 
c  k            0.71845E-02     150   0.19778E-03   0.33378E-05 0.20289E+01 
c  epsilon      0.20465E+02      98   0.34535E-03   0.29082E+02 0.56060E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.5713e-05                            11
a  epsilon               -0.054855                            15
a  Local Time Step      4.2278e-08                        280820


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0724          2.2334         0.22185         0.05015
v  Velocity[Y]             -2.3003          3.1424         0.14805         0.12018
v  Velocity[Z]             -3.8669          2.6358    
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7545      2.3894e+06          258.95          13.415


 TIME FOR THE TIME STEP               80:        0.15252E+03

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


 INSTANT    0.810000000E+01   TIME STEP NUMBER              81
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Sm
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7545      2.3894e+06          258.95          13.415


 TIME FOR THE TIME STEP               80:        0.16839E+03

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


 INSTANT    0.810000000E+01   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         0.170718928E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491635E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38015E+00 0.88837E+00
   Friction velocity        uet   :  0.55118E-02 0.42953E+01
   Friction velocity        uk    :  0.55116E-02 0.42953E+01
   Dimensionless distance   yplus :  0.23334E-03 0.68712E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        580
   Nb of faces within the viscous sub-layer     :      33810
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24602E+00     279   0.11257E+00   0.26788E-01 0.15661E+01 
c  Velocity[X]                                      0.68465E-02 
c  Velocity[Y]                                      0.91699E-02 
c  Velocity[Z]                                      0.10771E-01 
c  Pressure     0.82618E-02     834   0.12081E-01   0.40825E-01 0.21231E-01 
c  k            0.71868E-02     151   0.20086E-03   0.30583E-05 0.19459E+01 
c  epsilon      0.20490E+02      97   0.23480E-03   0.20080E+02 0.46573E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.6455e-05                            13
a  epsilon               -0.064918                            16
a  Local Time Step      4.2278e-08                        280822


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0685          2.2373         0.22182        0.050112
v  Velocity[Y]             -2.2921           2.947         0.14806         0.12017
v  Velocity[Z]             -3.9682          2.6239        -0.11894     -0.00027459
v  ǁVelocityǁ           6.2285e-05          4.3158         0.73162         0.98675
v  Pressure                 -420.6          6803.8          4463.9          3709.9
v  k                    2.2979e-09         0.15426       0.0015847       0.0045448
v  epsilon              1.3146e-05            1014          2.2162          1.5201
v  TurbVisc             2.2325e-14         0.11253      0.00033098       0.0043498
v  CourantNb             0.0012356           23467          41.712           10.67
v  FourierNb               0.22133      2.3653e+06          217.22          2.7457
v  total_pressure       4.9958e+05       5.068e+05      5.0446e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010143


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7582      2.3888e+06          258.93          13.416


 TIME FOR THE TIME STEP               81:        0.15774E+03

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


 INSTANT    0.820000000E+01   TIME STEP NUMBER              82
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.163876224E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491796E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38295E+00 0.88688E+00
   Friction velocity        uet   :  0.81916E-02 0.43735E+01
   Friction velocity        uk    :  0.81696E-02 0.43735E+01
   Dimensionless distance   yplus :  0.53565E-03 0.69977E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        578
   Nb of faces within the viscous sub-layer     :      33805
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-------------------------------------------------------a  k                    -1.284e-05                            10
a  epsilon               -0.043886                            11
a  Local Time Step      4.2278e-08                        280820


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0717          2.2405          0.2217        0.050108
v  Velocity[Y]              -2.295          3.1636         0.14807          0.1202
v  Velocity[Z]             -3.9537          2.6394        -0.11907     -0.00025972
v  ǁVelocityǁ           7.7803e-05          4.3027          0.7317         0.98675
v  Pressure                -423.97          6801.9          4462.4          3708.8a  k                    -1.284e-05                            10
a  epsilon               -0.043886                            11
a  Local Time Step      4.2278e-08                        280820


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0717          2.2405          0.2217        0.050108
v  Velocity[Y]              -2.295          3.1636         0.14807          0.1202
v  Velocity[Z]             -3.9537          2.6394        -0.11907     -0.00025972
v  ǁVelocityǁ           7.7803e-05          4.3027          0.7317         0.98675
v  Pressure                -423.97          6801.9          4462.4          3708.8
v  k                    2.4009e-09         0.15518       0.0015851       0.0045452
v  epsilon              1.3122e-05          1023.8          2.2156          1.5209
v  TurbVisc             1.9694e-14         0.11253      0.00033103       0.0043499
v  CourantNb             0.0093777           22962          41.689           10.67
v  FourierNb               0.22133      2.3653e+06          217.22          2.7459
v  total_pressure       4.9958e+05       5.068e+05      5.0446e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010144


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7551      2.3882e+06          258.91          13.416


 TIME FOR THE TIME STEP               82:        0.15612E+03

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


 INSTANT    0.830000000E+01   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        -0.476347411E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491799E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37670E+00 0.88602E+00
   Friction velocity        uet   :  0.58376E-02 0.37661E+01
   Friction velocity        uk    :  0.58373E-02 0.37661E+01
   Dimensionless distance   yplus :  0.45193E-03 0.68795E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        578
   Nb of faces within the viscous sub-layer     :      33810
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24608E+00     290   0.11549E+00   0.27373E-01 0.15829E+01 
c  Velocity[X]                                      0.73201E-02 
c  Velocity[Y]                                      0.93661E-02 
c  Velocity[Z]                                      0.10687E-01 
c  Pressure     0.83725E-02     726   0.12272E-01   0.41352E-01 0.16682E-01 
c  k            0.71885E-02     146   0.21566E-03   0.39477E-05 0.22023E+01 
c  epsilon      0.20503E+02      94   0.31218E-03   0.58624E+02 0.79576E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00026659                            15
a  epsilon                -0.47728                            18
a  Local Time Step      4.2278e-08                        280814


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0798          2.2362         0.22172        0.050095
v  Velocity[Y]             -2.2906            2.95         0.14813         0.12023
v  Velocity[Z]             -3.8885          2.6348        -0.11897     -0.00025221
v  ǁVelocityǁ           0.00012151          4.2327         0.73173         0.98681
v  Pressure                -424.88          6801.3          4461.8          3708.3
v  k                    2.5417e-09         0.15508       0.0015822       0.0045446
v  epsilon              1.3099e-05            1022            2.21          1.5193
v  TurbVisc             2.2461e-14         0.11253       0.0003311       0.0043498
v  CourantNb              0.010067           24460          41.699           10.67
v  FourierNb               0.22133      2.3653e+06          217.22          2.7455
v  total_pressure       4.9958e+05       5.068e+05      5.0446e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010141


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7554      2.3897e+06          258.92          13.416


 TIME FOR THE TIME STEP               83:        0.16068E+03

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


 INSTANT    0.840000000E+01   TIME STEP NUMBER              84
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.314522541E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+0   Dimensionless distance   yplus :  0.45692E-03 0.69896E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        577
   Nb of faces within the viscous sub-layer     :      33806
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24601E+00     282   0.11412E+00   0.28716E-01 0.16214E+01 
c  Velocity[X]                                      0.76688E-02 
c  Velocity[Y]                     Dimensionless distance   yplus :  0.45692E-03 0.69896E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        577
   Nb of faces within the viscous sub-layer     :      33806
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24601E+00     282   0.11412E+00   0.28716E-01 0.16214E+01 
c  Velocity[X]                                      0.76688E-02 
c  Velocity[Y]                                      0.99285E-02 
c  Velocity[Z]                                      0.11118E-01 
c  Pressure     0.86279E-02     579   0.12605E-01   0.42622E-01 0.10079E-01 
c  k            0.71884E-02     147   0.24392E-03   0.39517E-05 0.22111E+01 
c  epsilon      0.20493E+02      94   0.35183E-03   0.40166E+02 0.65852E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.2641e-05                             9
a  epsilon               -0.041342                            13
a  Local Time Step      4.2278e-08                        280808


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0705          2.2438          0.2218        0.050113
v  Velocity[Y]             -2.2944          3.1466         0.14816          0.1202
v  Velocity[Z]             -3.8816          2.6341        -0.11912     -0.00026599
v  ǁVelocityǁ           6.6789e-05          4.2293         0.73183         0.98674
v  Pressure                -424.73          6801.5            4462          3708.4
v  k                    2.3371e-09         0.15493       0.0015855       0.0045457
v  epsilon               1.161e-05          1020.5          2.2192          1.5203
v  TurbVisc             2.2775e-14         0.11253      0.00033092       0.0043499
v  CourantNb            0.00078066           24118          41.708          10.671
v  FourierNb               0.22133      2.3653e+06          217.22          2.7461
v  total_pressure       4.9958e+05       5.068e+05      5.0446e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010143


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7563      2.3894e+06          258.93          13.417


 TIME FOR THE TIME STEP               84:        0.13681E+03

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


 INSTANT    0.850000000E+01   TIME STEP NUMBER              85
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.308564744E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491626E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38330E+00 0.88540E+00
   Friction velocity        uet   :  0.79733E-02 0.42326E+01
   Friction velocity        uk    :  0.79731E-02 0.42326E+01
   Dimensionless distance   yplus :  0.35314E-03 0.68789E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        577
   Nb of faces within the viscous sub-layer     :      33815
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24599E+00     279   0.11247E+00   0.27181E-01 0.15774E+01 
c  Velocity[X]                                      0.72029E-02 
c  Velocity[Y]                                      0.92779E-02 
c  Velocity[Z]                                      0.10700E-01 
c  Pressure     0.82593E-02     576   0.12070E-01   0.40791E-01 0.10968E-01 
c  k            0.71870E-02     149   0.19797E-03   0.38999E-05 0.21974E+01 
c  epsilon      0.20507E+02      97   0.32357E-03   0.53714E+02 0.76064E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0002497                            18
a  epsilon                -0.45393                            17
a  Local Time Step      4.2278e-08                        280812


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -1.078          2.2502         0.22178        0.050132
v  Velocity[Y]             -2.2933          2.9415         0.14826          0.1202
v  Velocity[Z]               -3.92          2.6319        -0.11913     -0.00026818
v  ǁVelocityǁ           0.00015429           4.264         0.73179         0.98682
v  Pressure                -425.82          6801.5            4462          3708.6
v  k                    2.3656e-09         0.15442       0.0015819       0.0045442
v  epsilon              1.3088e-05          1015.4          2.2131          1.5194
v  TurbVisc       INSTANT    0.860000000E+01   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        -0.904929866E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491634E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+0 INSTANT    0.860000000E+01   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        -0.904929866E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491634E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37761E+00 0.88690E+00
   Friction velocity        uet   :  0.85464E-02 0.38880E+01
   Friction velocity        uk    :  0.85357E-02 0.38880E+01
   Dimensionless distance   yplus :  0.49611E-03 0.69248E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        575
   Nb of faces within the viscous sub-layer     :      33814
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24602E+00     281   0.11590E+00   0.27276E-01 0.15801E+01 
c  Velocity[X]                                      0.72924E-02 
c  Velocity[Y]                                      0.91014E-02 
c  Velocity[Z]                                      0.10882E-01 
c  Pressure     0.84044E-02     699   0.12257E-01   0.41509E-01 0.12735E-01 
c  k            0.71865E-02     146   0.16940E-03   0.29571E-05 0.19136E+01 
c  epsilon      0.20481E+02      93   0.24336E-03   0.43350E+02 0.68494E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.3963e-05                            12
a  epsilon               -0.053357                            16
a  Local Time Step      4.2278e-08                        280816


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0742          2.2439         0.22183        0.050142
v  Velocity[Y]             -2.2969          3.1569         0.14809         0.12021
v  Velocity[Z]             -3.9312          2.6245        -0.11903     -0.00022467
v  ǁVelocityǁ           4.8966e-05          4.2702         0.73175         0.98682
v  Pressure                -426.03          6801.7          4461.5          3708.3
v  k                    2.4858e-09         0.15564        0.001579       0.0045444
v  epsilon              1.3108e-05          1026.5          2.2034          1.5185
v  TurbVisc             2.1586e-14         0.11253      0.00033074       0.0043498
v  CourantNb              0.002533           24147          41.704          10.672
v  FourierNb               0.22132      2.3653e+06          217.22          2.7461
v  total_pressure       4.9957e+05       5.068e+05      5.0446e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010142


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7622      2.3894e+06          258.93          13.418


 TIME FOR THE TIME STEP               86:        0.13752E+03

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


 INSTANT    0.870000000E+01   TIME STEP NUMBER              87
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.660812291E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491785E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38040E+00 0.88337E+00
   Friction velocity        uet   :  0.93654E-02 0.39843E+01
   Friction velocity        uk    :  0.93453E-02 0.39843E+01
   Dimensionless distance   yplus :  0.29195E-03 0.68822E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        574
   Nb of faces within the viscous sub-layer     :      33816
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24605E+00     286   0.11535E+00   0.27900E-01 0.15982E+01 
c  Velocity[X]                                      0.74233E-02 
c  Velocity[Y]                                      0.97015E-02 
c  Velocity[Z]                                      0.10775E-01 
c  Pressure     0.84500E-02     819   0.12292E-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -1.078           2.237         0.22172        0.050126
v  Velocity[Y]             -2.2875          2.9652         0.14817         0.12017
v  Velocity[Z]             -3.8453          2.6234        -0.11885     -0.00023574
v  ǁVelocityǁ           8.8607e-05          4.1963         0.73151         0.98679
v  Pressure                -424.08          6803.1          4462.9          3709.4
v  k                    2.5236e-09         0.15416       0.0015791       0.0045446
v  epsilon              1.3138e-05          1012.6          2.2026          1.5187
v  TurbVisc             2.2786e-14         0.11253      0.00033078       0.0043499
v  CourantNb              0.013752           23778          41.695          10.673
v  Fouri-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -1.078           2.237         0.22172        0.050126
v  Velocity[Y]             -2.2875          2.9652         0.14817         0.12017
v  Velocity[Z]             -3.8453          2.6234        -0.11885     -0.00023574
v  ǁVelocityǁ           8.8607e-05          4.1963         0.73151         0.98679
v  Pressure                -424.08          6803.1          4462.9          3709.4
v  k                    2.5236e-09         0.15416       0.0015791       0.0045446
v  epsilon              1.3138e-05          1012.6          2.2026          1.5187
v  TurbVisc             2.2786e-14         0.11253      0.00033078       0.0043499
v  CourantNb              0.013752           23778          41.695          10.673
v  FourierNb               0.22132      2.3653e+06          217.22          2.7454
v  total_pressure       4.9958e+05       5.068e+05      5.0446e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010142


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7577      2.3891e+06          258.92          13.418


 TIME FOR THE TIME STEP               87:        0.14769E+03

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


 INSTANT    0.880000000E+01   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        -0.365364102E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491620E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38442E+00 0.88633E+00
   Friction velocity        uet   :  0.57602E-02 0.37266E+01
   Friction velocity        uk    :  0.57532E-02 0.37266E+01
   Dimensionless distance   yplus :  0.45046E-03 0.68964E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        581
   Nb of faces within the viscous sub-layer     :      33814
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24602E+00     291   0.11487E+00   0.27532E-01 0.15876E+01 
c  Velocity[X]                                      0.72053E-02 
c  Velocity[Y]                                      0.95511E-02 
c  Velocity[Z]                                      0.10775E-01 
c  Pressure     0.82408E-02     646   0.12037E-01   0.40718E-01 0.11219E-01 
c  k            0.71827E-02     153   0.22004E-03   0.35927E-05 0.21096E+01 
c  epsilon      0.20453E+02      99   0.35822E-03   0.35338E+02 0.61909E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00024712                            15
a  epsilon                -0.43846                            16
a  Local Time Step      4.2278e-08                        280819


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0703           2.243         0.22177        0.050125
v  Velocity[Y]                -2.3          3.1447         0.14809         0.12018
v  Velocity[Z]             -3.9563          2.6367        -0.11901     -0.00025964
v  ǁVelocityǁ           8.1967e-05          4.3083         0.73161         0.98682
v  Pressure                -421.97          6803.3          4463.2          3709.3
v  k                    2.4939e-09         0.15509       0.0015823       0.0045442
v  epsilon              1.2365e-05            1022          2.2107          1.5179
v  TurbVisc              2.278e-14         0.11253      0.00033068       0.0043499
v  CourantNb             0.0016334           22106          41.655          10.671
v  FourierNb               0.22132      2.3653e+06          217.22          2.7452
v  total_pressure       4.9958e+05       5.068e+05      5.0446e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010141


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7617      2.3874e+06          258.88          13.416


 TIME FOR THE TIME STEP               88:        0.13395E+03

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


 INSTANT    0.890000000E+01   TIME STEP NUMBER              89
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.764311783E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491634E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0     ------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24607E+00     288   0.11649E+00   0.27331E-01 0.15816E+01 
c  Velocity[X]                                      0.70621E-02 
c  Velocity[Y]                                      0.91648E-02 
c  Velocity[Z]                                      0.11104E-01 
c  Pressure     0.81052E-02     467   0.11825E-01   0.40041E-01 0.10736E-01 
c  k            0.71915E-02     148   0.20728E-03   0.36122E-05 0.21147E+01 
c  epsilon      0.20551E+02      93   0.40230E-03 ------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24607E+00     288   0.11649E+00   0.27331E-01 0.15816E+01 
c  Velocity[X]                                      0.70621E-02 
c  Velocity[Y]                                      0.91648E-02 
c  Velocity[Z]                                      0.11104E-01 
c  Pressure     0.81052E-02     467   0.11825E-01   0.40041E-01 0.10736E-01 
c  k            0.71915E-02     148   0.20728E-03   0.36122E-05 0.21147E+01 
c  epsilon      0.20551E+02      93   0.40230E-03   0.59750E+02 0.80122E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.4533e-05                            13
a  epsilon               -0.036579                            14
a  Local Time Step      4.2278e-08                        280816


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0724          2.2471         0.22193        0.0------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24607E+00     288   0.11649E+00   0.27331E-01 0.15816E+01 
c  Velocity[X]                                      0.70621E-02 
c  Velocity[Y]                                      0.91648E-02 
c  Velocity[Z]                                      0.11104E-01 
c  Pressure     0.81052E-02     467   0.11825E-01   0.40041E-01 0.10736E-01 
c  k            0.71915E-02     148   0.20728E-03   0.36122E-05 0.21147E+01 
c  epsilon      0.20551E+02      93   0.40230E-03   0.59750E+02 0.80122E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.4533e-05                            13
a  epsilon               -0.036579                            14
a  Local Time Step      4.2278e-08                        280816


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0724          2.2471         0.22193        0.050137
v  Velocity[Y]             -2.2883          2.9509         0.14814         0.12016
v  Velocity[Z]             -3.8894          2.6255        -0.11895     -0.00026753
v  ǁVelocityǁ           0.00017606           4.225         0.73183         0.98689
v  Pressure                -419.31          6803.6          4463.1          3709.3
v  k                    2.5691e-09         0.15514        0.001583       0.0045444
v  epsilon              1.3207e-05          1022.8          2.2166          1.5197
v  TurbVisc             2.2442e-14         0.11253      0.00033079       0.0043499
v  CourantNb             0.0042243           25342          41.679          10.672
v  FourierNb               0.22132      2.3653e+06          217.22          2.7452
v  total_pressure       4.9958e+05       5.068e+05      5.0446e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023         0.01014


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7578      2.3906e+06           258.9          13.417


 TIME FOR THE TIME STEP               89:        0.12594E+03

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


 INSTANT    0.900000000E+01   TIME STEP NUMBER              90
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.574046436E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491784E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37726E+00 0.88714E+00
   Friction velocity        uet   :  0.49672E-02 0.38244E+01
   Friction velocity        uk    :  0.49638E-02 0.38244E+01
   Dimensionless distance   yplus :  0.36389E-03 0.68865E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        580
   Nb of faces within the viscous sub-layer     :      33810
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24606E+00     279   0.11482E+00   0.27729E-01 0.15931E+01 
c  Velocity[X]                                      0.71560E-02 
c  Velocity[Y]                                      0.95369E-02 
c  Velocity[Z]                                      0.11036E-01 
c  Pressure     0.82731E-02     700   0.12090E-01   0.40860E-01 0.11799E-01 
c  k            0.71946E-02     142   0.21610E-03   0.32111E-05 0.19936E+01 
c  Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.133176400E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491785E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ----------------------------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.133176400E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491785E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38252E+00 0.88260E+00
   Friction velocity        uet   :  0.86830E-02 0.33344E+01
   Friction velocity        uk    :  0.86720E-02 0.33344E+01
   Dimensionless distance   yplus :  0.37611E-03 0.69687E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        579
   Nb of faces within the viscous sub-layer     :      33817
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
--------------------------------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.133176400E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491785E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38252E+00 0.88260E+00
   Friction velocity        uet   :  0.86830E-02 0.33344E+01
   Friction velocity        uk    :  0.86720E-02 0.33344E+01
   Dimensionless distance   yplus :  0.37611E-03 0.69687E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        579
   Nb of faces within the viscous sub-layer     :      33817
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24611E+00     287   0.11465E+00   0.26989E-01 0.15717E+01 
c  Velocity[X]                                      0.70999E-02 
c  Velocity[Y]                                      0.92754E-02 
c  Velocity[Z]                                      0.10614E-01 
c  Pressure     0.81626E-02     666   0.11941E-01   0.40322E-01 0.11381E-01 
c  k            0.71882E-02     145   0.17646E-03   0.30825E-05 0.19538E+01 
c  epsilon      0.20511E+02      92   0.27464E-03   0.37613E+02 0.63745E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00023577                            15
a  epsilon                -0.43243                            17
a  Local Time Step      4.2278e-08                        280815


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0846          2.2441         0.22171        0.050159
v  Velocity[Y]             -2.2867          2.9489          0.1481         0.12018
v  Velocity[Z]             -3.9679          2.6308        -0.11889     -0.00025185
v  ǁVelocityǁ           5.0434e-05          4.3159         0.73168          0.9869
v  Pressure                -416.81          6802.7          4462.3          3708.8
v  k                    2.5272e-09         0.15422       0.0015791       0.0045439
v  epsilon              1.3237e-05          1011.6          2.2025          1.5183
v  TurbVisc             2.2463e-14         0.11253      0.00033078       0.0043499
v  CourantNb             0.0095292           24208          41.692          10.674
v  FourierNb               0.22132      2.3653e+06          217.22          2.7453
v  total_pressure       4.9958e+05       5.068e+05      5.0446e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010143


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7605      2.3895e+06          258.91          13.419


 TIME FOR THE TIME STEP               91:        0.12754E+03

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


 INSTANT    0.920000000E+01   TIME STEP NUMBER              92
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.118348309E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491783E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   v  Velocity[Z]             -3.9464          2.6302        -0.11907     -0.00025355
v  ǁVelocityǁ           6.1792e-05          4.2967         0.73181         0.98687
v  Pressure                -417.98          6800.9          4460.8          3707.5
v  k                    2.5586e-09         0.15433       0.0015851       0.0045448
v  epsilon              1.3223e-05          1012.6          2.2198          1.5197
v  TurbVisc             2.2783e-14         0.11253      0.00033066       0.0043499
v  CourantNb            0.00034382           22388          41.669          10.673
v  FourierNb               0.22132      2.3653e+06          217.22          2.7458
v  total_pressure       4.9958e+05       5.068e+05      5.0446e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010143


  ** Cv  Velocity[Z]             -3.9464          2.6302        -0.11907     -0.00025355
v  ǁVelocityǁ           6.1792e-05          4.2967         0.73181         0.98687
v  Pressure                -417.98          6800.9          4460.8          3707.5
v  k                    2.5586e-09         0.15433       0.0015851       0.0045448
v  epsilon              1.3223e-05          1012.6          2.2198          1.5197
v  TurbVisc             2.2783e-14         0.11253      0.00033066       0.0043499
v  CourantNb            0.00034382           22388          41.669          10.673
v  FourierNb               0.22132      2.3653e+06          217.22          2.7458
v  total_pressure       4.9958e+05       5.068e+05      5.0446e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010143


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7629      2.3877e+06          258.89          13.419


 TIME FOR THE TIME STEP               92:        0.14264E+03

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


 INSTANT    0.930000000E+01   TIME STEP NUMBER              93
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet         v  Velocity[Z]             -3.9464          2.6302        -0.11907     -0.00025355
v  ǁVelocityǁ           6.1792e-05          4.2967         0.73181         0.98687
v  Pressure                -417.98          6800.9          4460.8          3707.5
v  k                    2.5586e-09         0.15433       0.0015851       0.0045448
v  epsilon              1.3223e-05          1012.6          2.2198          1.5197
v  TurbVisc             2.2783e-14         0.11253      0.00033066       0.0043499
v  CourantNb            0.00034382           22388          41.669          10.673
v  FourierNb               0.22132      2.3653e+06          217.22          2.7458
v  total_pressure       4.9958e+05       5.068e+05      5.0446e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010143


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7629      2.3877e+06          258.89          13.419


 TIME FOR THE TIME STEP               92:        0.14001E+03

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


 INSTANT    0.930000000E+01   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        -0.282350522E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491786E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37679E+00 0.88375E+00
   Friction velocity        uet   :  0.86802E-02 0.46377E+01
   Friction velocity        uk    :  0.86623E-02 0.46377E+01
   Dimensionless distance   yplus :  0.28981E-03 0.69262E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        582
   Nb of faces within the viscous sub-layer     :      33816
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24607E+00     284   0.11555E+00   0.27243E-01 0.15791E+01 
c  Velocity[X]                                      0.73496E-02 
c  Velocity[Y]                                      0.94682E-02 
c  Velocity[Z]                                      0.10425E-01 
c  Pressure     0.82165E-02     778   0.12002E-01   0.40591E-01 0.17440E-01 
c  k            0.71931E-02     139   0.17456E-03   0.27294E-05 0.18384E+01 
c  epsilon      0.20542E+02      96   0.23061E-03   0.20403E+02 0.46968E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.0553e-05                            13
a  epsilon               -0.095249                            13
a  Local Time Step      4.2278e-08                        280811


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.1048          2.2469         0.22172        0.050145
v  Velocity[Y]             -2.2839          2.9433         0.14808         0.12017
v  Velocity[Z]             -3.8803          2.6312        -0.11906     -0.00023809
v  ǁVelocityǁ           0.00014417          4.2181         0.73168         0.98687
v  Pressure                -419.62          6799.5          4459.8          3706.9
v  k                    2.5583e-09         0.15438       0.0015812       0.0045442
v  epsilon              2.0142e-06          1015.4          2.2077          1.5186
v  TurbVisc             2.2974e-14         0.11253      0.00033095       0.0043499
v  CourantNb             0.0062362           26168          41.708          10.673
v  FourierNb               0.22132      2.3653e+06          217.22          2.7457
v  total_pressure       4.9958e+05       5.068e+05      5.0446e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010-----------------------------------------------------------------------------
c  Velocity     0.24613E+00     292   0.11622E+00   0.27375E-01 0.15827E+01 
c  Velocity[X]                                      0.71421E-02 
c  Velocity[Y]                                      0.94894E-02 
c  Velocity[Z]                                      0.10743E-01 
c  Pressure     0.83793E-02     650   0.12268E-01   0.41402E-01 0.11379E-01 
c  k            0.71890E-02     135   0.16457E-03   0.22716E-05 0.16758E+01 
c  epsilon      0.20498E+02      90   0.23054E-03   0.17121E+02 0.42941E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  ---------------------------------------------------------------------------------
c  Velocity     0.24613E+00     292   0.11622E+00   0.27375E-01 0.15827E+01 
c  Velocity[X]                                      0.71421E-02 
c  Velocity[Y]                                      0.94894E-02 
c  Velocity[Z]                                      0.10743E-01 
c  Pressure     0.83793E-02     650   0.12268E-01   0.41402E-01 0.11379E-01 
c  k            0.71890E-02     135   0.16457E-03   0.22716E-05 0.16758E+01 
c  epsilon      0.20498E+02      90   0.23054E-03   0.17121E+02 0.42941E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.0698e-05                            13
a  epsilon               -0.052603                            15
a  Local Time Step      4.2278e-08                        280814


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0723          2.2366         0.22182        0.050146
v  Velocity[Y]             -2.2961          3.1825         0.14804         0.12019
v  Velocity[Z]             -3.8722          2.6384        -0.11914     -0.00023029
v  ǁVelocityǁ           0.00010689          4.2197         0.73179         0.98683
v  Pressure                -4-----------------------------------------------------------------------------
c  Velocity     0.24613E+00     292   0.11622E+00   0.27375E-01 0.15827E+01 
c  Velocity[X]                                      0.71421E-02 
c  Velocity[Y]                                      0.94894E-02 
c  Velocity[Z]                                      0.10743E-01 
c  Pressure     0.83793E-02     650   0.12268E-01   0.41402E-01 0.11379E-01 
c  k            0.71890E-02     135   0.16457E-03   0.22716E-05 0.16758E+01 
c  epsilon      0.20498E+02      90   0.23054E-03   0.17121E+02 0.42941E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.0698e-05                            13
a  epsilon               -0.052603                            15
a  Local Time Step      4.2278e-08                        280814


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0723          2.2366         0.22182        0.050146
v  Velocity[Y]             -2.2961          3.1825         0.14804         0.12019
v  Velocity[Z]             -3.8722          2.6384        -0.11914     -0.00023029
v  ǁVelocityǁ           0.00010689          4.2197         0.73179         0.98683
v  Pressure                -419.82          6799.7          4460.1          3706.9
v  k                    2.5272e-09         0.15493       0.0015813       0.0045444
v  epsilon               1.315e-05          1021.2           2.207           1.519
v  TurbVisc             2.2701e-14         0.11253      0.00033084         0.00435
v  CourantNb             0.0024633           22625          41.677          10.672
v  FourierNb               0.22132      2.3653e+06          217.22          2.7449
v  total_pressure       4.9958e+05       5.068e+05      5.0446e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010141


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7651      2.3879e+06           258.9          13.417


 TIME FOR THE TIME STEP               94:        0.12992E+03

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


 INSTANT    0.950000000E+01   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         0.870447473E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491618E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38403E+00 0.88657E+00
   Friction velocity        uet   :  0.86391E-02 0.46463E+01
   Friction velocity        uk    :  0.86386E-02 0.46463E+01
   Dimensionless distance   yplus :  0.38166E-03 0.69682E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        573
   Nb of faces within the viscous sub-layer     :      33820
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24609E+00     282   0.11500E+00   0.27119E-01 0.15755E+01 
c  Velocity[X]                                      0.72040E-02 
c  Velocity[Y]                                      0.91398E-02 
c  Velocity[Z]                                      0.10775E-01 
c  Pressure     0.82218E-02     590   0.12018E-01   0.40618E-01 0.14896E-01 
c  k            0.71941E-02     142   0.17464E-03   0.30597E-05 0.19462E+01 
c  epsilon      0.20588E+02      86   0.35164E-03   0.47945E+02 0.71787E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ----Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491777E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37863E+00 0.88595E+00
   Friction velocity        uet   :  0.72270E-02 0.36824E+01Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491777E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37863E+00 0.88595E+00
   Friction velocity        uet   :  0.72270E-02 0.36824E+01
   Friction velocity        uk    :  0.72266E-02 0.36824E+01
   Dimensionless distance   yplus :  0.32695E-03 0.68943E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        579
   Nb of faces within the viscous sub-layer     :      33803
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24607E+00     291   0.11253E+00   0.26900E-01 0.15692E+01 
c  Velocity[X]                                      0.71069E-02 
c  Velocity[Y]                                      0.93401E-02 
c  Velocity[Z]                                      0.10453E-01 
c  Pressure     0.82257E-02     832   0.11989E-01   0.40617E-01 0.30446E-01 
c  k            0.71946E-02     152   0.26587E-03   0.48625E-05 0.24530E+01 
c  epsilon      0.20541E+02      98   0.40586E-03   0.64267E+02 0.83286E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.2868e-05                            10
a  epsilon               -0.046375                            13
a  Local Time Step      4.2278e-08                        280809


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0829          2.2447         0.22184        0.050165
v  Velocity[Y]             -2.2933          2.9507         0.14805          0.1202
v  Velocity[Z]             -3.9366          2.6312        -0.11915     -0.00023959
v  ǁVelocityǁ           5.2296e-05          4.2784         0.73179         0.98684
v  Pressure                -424.16          6797.2          4458.3          3705.6
v  k                     2.501e-09          0.1547       0.0015874       0.0045467
v  epsilon              1.3054e-05            1018          2.2212          1.5211
v  TurbVisc             2.3346e-14         0.11253      0.00033091         0.00435
v  CourantNb             0.0015554           25997           41.69          10.673
v  FourierNb               0.22132      2.3653e+06          217.22          2.7457
v  total_pressure       4.9958e+05       5.068e+05      5.0446e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010141


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7673      2.3913e+06          258.91          13.419


 TIME FOR THE TIME STEP               96:        0.14286E+03

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


 INSTANT    0.970000000E+01   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         0.115214138E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491788E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38166E+00 0.88457E+00
   Friction velocity        uet   :  0.80818E-02 0.38308E+01
   Friction velocity        uk    :  0.80817E-02 0.38308E+01
   Dimensionless distance   yplus :  0.48881E-03 0.69161E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        579
   Nb of faces within the viscous sub-layer     :      33819
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24615E+00     272   0.11435E+00   0.26550E-01 0.15589E+01 
c  Velocity[X]                                      0.71437E-02 
c  Velocity[Y]                                      0.91095E-02 
c  Velocity[Z]                                      0.10297E-01 
c  Pressure     0.80603E-02     720   0.11762E-01   0.39766E-01 0.20123E-01 
c  k            0.71942E-02     144   0.16954E-03   0.32401E-05 0.20028E+01 
c  epsilon      0.20564E+02      92   0.23256E-03   0.23970E+02 0.50885E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00027427                            15
a  epsilon         v  epsilon              1.3026e-05          1017.8          2.2058          1.5186
v  TurbVisc             2.1692e-14         0.11253      0.00033129       0.0043503
v  CourantNb              0.010687           21350          41.676          10.672
v  FourierNb               0.22132      2.3653e+06          217.22          2.7451
v  total_pressure       4.9958e+05       5.068e+05      5.0446e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023         0.01014


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7662      2.3866e+06           258.9          13.417


 TIME FOR THE TIME STEP     v  epsilon              1.3026e-05          1017.8          2.2058          1.5186
v  TurbVisc             2.1692e-14         0.11253      0.00033129       0.0043503
v  CourantNb              0.010687           21350          41.676          10.672
v  FourierNb               0.22132      2.3653e+06          217.22          2.7451
v  total_pressure       4.9958e+05       5.068e+05      5.0446e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023         0.01014


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7662      2.3866e+06           258.9          13.417


 TIME FOR THE TIME STEP               97:        0.13448E+03

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


 INSTANT    0.980000000E+01   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         0.181193997E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491641E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38503E+00 0.88868E+00
   Friction velocity        uet   :  0.82322E-02 0.27782E+01
   Friction velocity        uk    :  0.82218E-02 0.27782E+01
   Dimensionless distance   yplus :  0.29436E-03 0.68970E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        583
   Nb of faces within the viscous sub-layer     :      33811
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24611E+00     293   0.11492E+00   0.27684E-01 0.15919E+01 
c  Velocity[X]                                      0.70398E-02 
c  Velocity[Y]                                      0.96860E-02 
c  Velocity[Z]                                      0.10958E-01 
c  Pressure     0.83432E-02     689   0.12199E-01   0.41199E-01 0.11874E-01 
c  k            0.71937E-02     132   0.16990E-03   0.20847E-05 0.16063E+01 
c  epsilon      0.20536E+02      88   0.20875E-03   0.16151E+02 0.41765E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.5101e-05                            12
a  epsilon               -0.045267                            18
a  Local Time Step      4.2278e-08                        280818


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0817          2.2443         0.22188        0.050165
v  Velocity[Y]             -2.2928          2.9297         0.14808         0.12019
v  Velocity[Z]             -3.9488          2.6309        -0.11911     -0.00023761
v  ǁVelocityǁ           2.0771e-05          4.3003         0.73188         0.98684
v  Pressure                -423.92          6797.9          4459.3          3706.5
v  k                    2.5296e-09         0.15614       0.0015823       0.0045456
v  epsilon              1.3005e-05          1031.7           2.207          1.5196
v  TurbVisc             2.2602e-14         0.11253      0.00033105       0.0043501
v  CourantNb            0.00045076           22934          41.683          10.672
v  FourierNb               0.22131      2.3653e+06          217.22          2.7458
v  total_pressure       4.9958e+05       5.068e+05      5.0446e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010141


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7671      2.3882e+06          258.91          13.418


 TIME FOR THE TIME STEP               98:        0.14210E+03

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


 INSTANT    0.990000000E+01   TIME STEP NUMBER              99
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.126586762E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491630E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37587E+00 0.88492E+00
   Friction velocity        uet   :  0.84600E-02 0.41689E+01
   Friction velocity        uk    :  0.84598E-02 0.41689E+01
   Dimensionless distance   yplusc  Velocity[Z]                                      0.10588E-01 
c  Pressure     0.82306E-02     541   0.11996E-01   0.40638E-01 0.96783E-02 
c  k            0.71977E-02     133   0.21868E-03   0.37353E-05 0.21499E+01 
c  epsilon      0.20591E+02      87   0.25593E-03   0.51891E+02 0.74656E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.1285e-05                            10
a  epsilon               -0.045598                            10
a  Local Time Step      4.2278e-08                        280823


  ** Computed fields on cells
   c  Velocity[Z]                                      0.10588E-01 
c  Pressure     0.82306E-02     541   0.11996E-01   0.40638E-01 0.96783E-02 
c  k            0.71977E-02     133   0.21868E-03   0.37353E-05 0.21499E+01 
c  epsilon      0.20591E+02      87   0.25593E-03   0.51891E+02 0.74656E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.1285e-05                            10
a  epsilon               -0.045598                            10
a  Local Time Step      4.2278e-08                        280823


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -1.093          2.2481         0.22159        0.050167
v  Velocity[Y]             -2.2885          2.9482         0.14821         0.12021
v  Velocity[Z]             -3.8923          2.6252        -0.11913     -0.00026793
v  ǁVelocityǁ           4.8203e-05          4.2322         0.73162         0.98688
v  Pressure                -425.07          6797.5          4459.1          3706.4
v  k                    2.4436e-09         0.15451       0.0015825       0.0045456
v  epsilon              1.3001e-05          1015.7          2.2102          1.5203
v  TurbVisc             2.2114e-14         0.11253      0.00033138       0.0043501
v  CourantNb              0.005227           21980          41.679          10.672
v  FourierNb               0.22132      2.3653e+06          217.22          2.7455
v  total_pressure       4.9957e+05       5.068e+05      5.0446e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010141


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7632      2.3873e+06           258.9          13.418


 TIME FOR THE TIME STEP               99:        0.13055E+03

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


 INSTANT    0.100000000E+02   TIME STEP NUMBER             100
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.174485272E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491781E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38148E+00 0.88404E+00
   Friction velocity        uet   :  0.84258E-02 0.34588E+01
   Friction velocity        uk    :  0.83997E-02 0.34588E+01
   Dimensionless distance   yplus :  0.40075E-03 0.68954E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        582
   Nb of faces within the viscous sub-layer     :      33810
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24611E+00     295   0.11285E+00   0.27164E-01 0.15769E+01 
c  Velocity[X]                                      0.74988E-02 
c  Velocity[Y]                                      0.92777E-02 
c  Velocity[Z]                                      0.10387E-01 
c  Pressure     0.82727E-02     445   0.12093E-01   0.40858E-01 0.11651E-01 
c  k            0.71927E-02     151   0.20601E-03   0.42299E-05 0.22882E+01 
c  epsilon      0.20535E+02      98   0.36740E-03   0.60719E+02 0.80970E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00024492                            16
a  epsilon                -0.43022                            19
a  Local Time Step      4.2278e-08                        280818


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0829          2.2638         0.22164        0.050171
v  Velocity[Y]             -2.2906          2.9358         0.14817         0.12021
v  Velocity[Z]             -3.8673          2.6367        -0.11922     -0.00027327
v  ǁVelocityǁ           3.3713e-05          4.2182         0.73171          0.9868
v  Pressure                -424.95          6797.7          4459.1          3706.2
v  k                    2.4778e-09          0.1545       0.0015851       0.0045458
v  epsilon              1.3022e-05          1015.9           2.217          1.5201
v  TurbVisc              2.184e-14         0.11253      0.00033123       0.0043502
v  CourantNb             0.0029485           24598          41.684          10.672
v  FourierNb               0.22132      2.3653e+06          217.22          2.7458
v  total_pressure       4.9958e+05       5.068e+05      5.0446e+05      5.0371e+05
v  Local Time Step            0.01         0.17319        0.010023        0.010141


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7654      2.3899e+06          258.91          13.418


 TIME FOR THE TIME STEP              100:        0.12720E+03

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


 IFree surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38308E+00 0.88403E+00
   Friction velocity        uet   :  0.56133E-02 0.32198E+01
   Friction velocity        uk    :  0.56130E-02 0.32198E+01
   Dimensionless distance   yplus :  0.28200E-03 0.69004E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        579
   Nb of facesFree surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38308E+00 0.88403E+00
   Friction velocity        uet   :  0.56133E-02 0.32198E+01
   Friction velocity        uk    :  0.56130E-02 0.32198E+01
   Dimensionless distance   yplus :  0.28200E-03 0.69004E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        579
   Nb of faces within the viscous sub-layer     :      33815
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26594E+00     296   0.10604E+00   0.16027E+02 0.28266E+02 
c  Velocity[X]                                      0.62347E+00 
c  Velocity[Y]                                      0.12786E+01 
c  Velocity[Z]                                      0.14125E+02 
c  Pressure     0.16309E-01    1804   0.59718E+00   0.80306E-01 0.66394E+02 
c  k            0.112Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38308E+00 0.88403E+00
   Friction velocity        uet   :  0.56133E-02 0.32198E+01
   Friction velocity        uk    :  0.56130E-02 0.32198E+01
   Dimensionless distance   yplus :  0.28200E-03 0.69004E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        579
   Nb of faces within the viscous sub-layer     :      33815
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26594E+00     296   0.10604E+00   0.16027E+02 0.28266E+02 
c  Velocity[X]                                      0.62347E+00 
c  Velocity[Y]                                      0.12786E+01 
c  Velocity[Z]                                      0.14125E+02 
c  Pressure     0.16309E-01    1804   0.59718E+00   0.80306E-01 0.66394E+02 
c  k            0.11233E-01     191   0.18972E-02   0.11924E-02 0.29089E+02 
c  epsilon      0.20562E+02     159   0.83246E-03   0.12767E+03 0.12153E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.6104e-07                             2
a  epsilon               -0.014842                             4
a  Local Time Step      4.2278e-08                        280819


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0794          3.9431         0.29318        0.072966
v  Velocity[Y]             -3.0689           5.209         0.23617         0.16993
v  Velocity[Z]             -5.8502          3.3482        -0.13673       0.0041616
v  ǁVelocityǁ             0.001146          6.8334         0.91124          1.3452
v  Pressure                 14.819           22364           12705           11800
v  k                    2.6968e-09         0.14768       0.0017679       0.0055075
v  epsilon              1.4584e-05          970.18          2.4415           1.616
v  TurbVisc              2.215e-14         0.11253      0.00033136       0.0043502
v  CourantNb             0.0013214           22992          41.683          10.672
v  FourierNb               0.22132      2.3653e+06          217.22          2.7453
v  total_pressure       5.0001e+05      5.2236e+05      5.1271e+05       5.118e+05
v  Local Time Step            0.01         0.17319        0.010023         0.01014


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7658      2.3883e+06          258.91          13.417


 TIME FOR THE TIME STEP              101:        0.20952E+03

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


 INSTANT    0.102000000E+02   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        -0.417341567E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640751E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12007E+01 0.15560E+01
   Friction velocity        uet   :  0.16045E-01 0.17494E+02
   Friction velocity        uk    :  0.15972E-01 0.17494E+02
   Dimensionless distance   yplus :  0.20878E-02 0.81205E+01
   ------------------------------------------------------
   Nb of reversv  FourierNb               0.22138      2.3653e+06          217.23          2.7505
v  total_pressure            5e+05      5.1903e+05      5.1159e+05      5.1022e+05
v  Local Time Step            0.01        0.092014        0.010004        0.010037


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.1776      2.3839e+06             275          18.082


 TIME FOR THE TIME STEP              102:        0.22822E+03

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


 INSTANT    0.103000000E+02   TIME STEP NUMBER             103
 ============================================================= 




   ** BOUNDARY MASv  FourierNb               0.22138      2.3653e+06          217.23          2.7505
v  total_pressure            5e+05      5.1903e+05      5.1159e+05      5.1022e+05
v  Local Time Step            0.01        0.092014        0.010004        0.010037


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.1776      2.3839e+06             275          18.082


 TIME FOR THE TIME STEP              102:        0.23092E+03

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


 INSTANT    0.103000000E+02   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         0.543376351E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640918E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------v  FourierNb               0.22138      2.3653e+06          217.23          2.7505
v  total_pressure            5e+05      5.1903e+05      5.1159e+05      5.1022e+05
v  Local Time Step            0.01        0.092014        0.010004        0.010037


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.1776      2.3839e+06             275          18.082


 TIME FOR THE TIME STEP              102:        0.22946E+03

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


 INSTANT    0.103000000E+02   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         0.543376351E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640918E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10605E+01 0.18052E+01
   Friction velocity        uet   :  0.10766E-01 0.26345E+02
   Friction velocity        uk    :  0.10740E-01 0.26345E+02
   Dimensionless distance   yplus :  0.33616E-02 0.87931E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2365
   Nb of faces within the viscous sub-layer     :      31561
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46252E+00     479   0.10984E+00   0.71871E+00 0.52002E+01 
c  Velocity[X]                                      0.16688E+00 
c  Velocity[Y]                                      0.27146E+00 
c  Velocity[Z]                                      0.28037E+00 
c  Pressure     0.71301E-01    1842   0.31203E+00   0.29763E+00 0.34079E+02 
c  k            0.15746E-01     178   0.38351E-02   0.20478E-02 0.30839E+02 
c  epsilon      0.28095E+03      99   0.43075E-02   0.75029E+06 0.27438E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0005975                           543
a  epsilon                 -4.5947                           645
a  Local Time Step      4.2278e-08                        281328


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.3108          3.4585         0.31816        0.081638
v  Velocity[Y]             -2.8516          4.8595         0.28237         0.19707
v  Velocity[Z]             -5.3326          3.9086        -0.14437        0.011084
v  ǁVelocityǁ            0.0011171           6.622          1.0111          1.5579
v  Pressure                -24.729           13476          9037.2          7398.2
v  k                    1.3639e-09         0.58923       0.0024783       0.0071912
v  epsilon              4.4873e-06           16634          6.0236          2.8175
v  TurbVisc             2.6195e-14         0.14195      0.00038965       0.0057923
v  CourantNb              0.011656           45941          58.868          15.612
v  FourierNb               0.22138      2.3653e+06          217.24          2.7481
v  total_pressure       4.9998e+05      5.1348e+05      5.0904e+05       5.074e+05
v  Local Time Step            0.01        0.068942        0.010005        0.010042


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2848      2.3976e+06          276.11           18.36


 TIME FOR THE TIME STEP              103:        0.21763E+03

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


 INSTANT    0.104000000E+02   TIME STEP NUMBER             104
 ============================================================= 




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

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00052014                            72
a  epsilon                 -7.8838                           163
a  Local Time Step      4.2278e-08                        281458


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.4108          3.4527         0.32139        0.080225
v  Velocity[Y]              -2.952          5.1781          0.2742         0.19286
v  Velocity[Z]              -5.379          3.7986         -0.1646      0.00055431
v  ǁVelocityǁ           0.00081873          6.4925          1.0309          1.5391
v  Pressure                -806.96           11591          7819.5          6169.8
v  k                    1.3989e-09         0.42881       0.0028776       0.0073845
v  epsilon              1.5362e-07           10891          6.9496          3.0912
v  TurbVisc              1.036e-14          0.1418      0.00036412       0.0059714
v  CourantNb              0.013412           43006          59.968          15.848
v  FourierNb               0.22136      2.3653e+06          217.21          2.7459
v  total_pressure       4.9919e+05      5.1159e+05      5.0782e+05      5.0617e+05
v  Local Time Step            0.01        0.057755        0.010004        0.010043


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.3024      2.3676e+06          277.17          18.594


 TIME FOR THE TIME STEP              104:        0.22674E+03

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


 INSTANT    0.105000000E+02   TIME STEP NUMBER             105
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
-------------------------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00052014                            72
a  epsilon                 -7.8838                           163
a  Local Time Step      4.2278e-08                        281458


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.4108          3.4527         0.32139        0.080225
v  Velocity[Y]              -2.952          5.1781          0.2742         0.19286
v  Velocity[Z]              -5.379          3.7986         -0.1646      0.00055431
v  ǁVelocityǁ           0.00081873          6.4925          1.0309          1.5391
v  Pressure                -806.96           11591          7819.5          6169.8
v  k                    1.3989e-09         0.42881       0.0028776       0.0073845
v  epsilon              1.5362e-07           10891          6.9496          3.0912
v  TurbVisc              1.036e-14          0.1418      0.00036412       0.0059714
v  CourantNb              0.013412           43006          59.968          15.848
v  FourierNb               0.22136      2.3653e+06          217.21          2.7459
v  total_pressure       4.9919e+05      5.1159e+05      5.0782e+05      5.0617e+05
v  Local Time Step            0.01        0.057755        0.010004        0.010043


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.3024      2.3676e+06          277.17          18.594


 TIME FOR THE TIME STEP              104:        0.23628E+03

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


 INSTANT    0.105000000E+02   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         0.425578390E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640925E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11655E+01 0.17706E+01
   Friction velocity        uet   :  0.15991E-01 0.28035E+02
   Friction velocity        uk    :  0.15985E-01 0.28035E+02
   Dimensionless distance   yplus :  0.35773E-02 0.89735E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2345
   Nb of faces within the viscous sub-layer     :      30978
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41606E+00     455   0.12522E+00   0.50924E+00 0.44678E+01 
c  Velocity[X]                                      0.10381E+00 
c  Velocity[Y]                                      0.16180E+00 
c  Velocity[Z]                                      0.24362E+00 
c  Pressure     0.74806E-01    1027   0.14867E+00   0.26803E+00 0.20713E+01 
c  k            0.15349E-01     178   0.88826E-03   0.14671E-03 0.80982E+01 
c  epsilon      0.22666E+03     126   0.11100E-02   0.94473E+04 0.33206E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0005867                            21
a  epsilon                 -2.9947                            63
a  Local Time Step      4.2278e-08                        281462


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -1.462      ------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12222E+01 0.17499E+01
   Friction velocity        uet   :  0.14185E-01 0.27737E+02
   Friction velocity        uk    :  0.14172E-01 0.27737E+02
   Dimensionless distance   yplus :  0.35392E-02 0.90741E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2334
   Nb of faces within the viscous sub-layer     :      30798
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41125E+00     438   0.13312E+00   0.38605E+00 0.38876E+01 
c  Velocity[X]                                      0.10157E+00 
c  Velocity[Y]                                      0.14403E+00 
c  Velocity[Z]                                      0.14045E+00 
c  Pressure     0.59231E-01    1590   0.11652E+00   0.19963E+00 0.67332E+01 
c  k            0.15177E-01     187   0.76989E-03   0.91549E-04 0.63641E+01 
c  epsilon      0.19894E+03     294   0.53028E-03   0.37119E+04 0.21854E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.7267e-07                             2
a  epsilon              -0.0003877                             1
a  Local Time Step      4.2278e-08                        281453


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.4759          3.3718         0.32817        0.079504
v  Velocity[Y]             -3.1623          5.1737         0.25389         0.18864
v  Velocity[Z]             -5.5353          3.8546        -0.17494      -0.0038622
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12222E+01 0.17499E+01
   Friction velocity        uet   :  0.14185E-01 0.27737E+02
   Friction velocity        uk    :  0.14172E-01 0.27737E+02
   Dimensionless distance   yplus :  0.35392E-02 0.90741E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2334
   Nb of faces within the viscous sub-layer     :      30798
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41125E+00     438   0.13312E+00   0.38605E+00 0.38876E+01 
c  Velocity[X]                                      0.10157E+00 
c  Velocity[Y]                                      0.14403E+00 
c  Velocity[Z]                                      0.14045E+00 
c  Pressure     0.59231E-01    1590   0.11652E+00   0.19963E+00 0.67332E+01 
c  k            0.15177E-01     187   0.76989E-03   0.91549E-04 0.63641E+01 
c  epsilon      0.19894E+03     294   0.53028E-03   0.37119E+04 0.21854E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.7267e-07                             2
a  epsilon              -0.0003877                             1
a  Local Time Step      4.2278e-08                        281453


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.4759          3.3718         0.32817        0.079504
v  Velocity[Y]             -3.1623          5.1737         0.25389         0.18864
v  Velocity[Z]             -5.5353          3.8546        -0.17494      -0.0038622
v  ǁVelocityǁ            0.0036845          6.3817          1.0665          1.5251
v  Pressure                -685.15           12346          8285.4          6758.6
v  k                    5.5259e-09         0.35364       0.0030769       0.0075137
v  epsilon              2.0895e-05            9189          7.0524          3.1685
v  TurbVisc             4.2026e-14         0.14179      0.00039819       0.0062028
v  CourantNb             0.0053005           64050          61.892          16.132
v  FourierNb               0.22134      2.3653e+06          217.23          2.7511
v  total_pressure       4.9931e+05      5.1235e+05      5.0829e+05      5.0676e+05
v  Local Time Step            0.01        0.069884        0.010004         0.01004


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0998      2.4293e+06          279.12          18.883


 TIME FOR THE TIME STEP              106:        0.20954E+03

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


 INSTANT    0.107000000E+02   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        -0.312484825E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640700E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12125E+01 0.17236E+01
   Friction velocity        uet   :  0.10250E-01 0.29766E+02
   Friction velocity        uk    :  0.10240E-01 0.29766E+02
   Dimensionless distance   yplus :  0.37981E-02 0.90554E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2343
   Nb of faces within the viscous sub-layer     :      30642
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-------------
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0954      2.4383e+06          280.48          19.026


 TIME FOR THE TIME STEP              107:        0.20512E+03

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


 INSTANT    0.108000000E+02   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         0.261445492E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640668E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12473E+01 0.16866E+01
   Friction velocity        uet   :  0.12292E-01 0.32113E+02
   Friction velocity        uk    :  0.12259E-01 0.32113E+02
   Dimensionless distance   yplus :  0.40976E-02 0.91142E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2368
   Nb of faces within the viscous sub-layer     :      30522
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
------------------------------------------------------------------
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0954      2.4383e+06          280.48          19.026


 TIME FOR THE TIME STEP              107:        0.20578E+03

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


 INSTANT    0.108000000E+02   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         0.261445492E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640668E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12473E+01 0.16866E+01
   Friction velocity        uet   :  0.12292E-01 0.32113E+02
   Friction velocity        uk    :  0.12259E-01 0.32113E+02
   Dimensionless distance   yplus :  0.40976E-02 0.91142E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2368
   Nb of faces within the viscous sub-layer     :      30522
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41795E+00     411   0.13579E+00   0.27023E+00 0.32152E+01 
c  Velocity[X]                                      0.64121E-01 
c  Velocity[Y]                                      0.11155E+00 
c  Velocity[Z]                                      0.94558E-01 
c  Pressure     0.48168E-01    1505   0.84731E-01   0.14713E+00 0.31637E+01 
c  k            0.14981E-01     179   0.98778E-03   0.89243E-04 0.62341E+01 
c  epsilon      0.15728E+03     223   0.59539E-03   0.61255E+04 0.30793E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.6554e-05                             8
a  epsilon                -0.54576                            11
a  Local Time Step      4.2278e-08                        281422


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.5136          3.3569         0.33443         0.07975
v  Velocity[Y]             -3.2637          5.0218         0.24326          0.1899
v  Velocity[Z]             -5.5852          3.8224        -0.17598     -0.00090451
v  ǁVelocityǁ           0.00095595           6.304          1.1032          1.5424
v  Pressure                -359.04           13331          9018.9          7420.3
v  k                    8.1928e-09         0.31961       0.0032917       0.0076471
v  epsilon               1.605e-05            7526          7.5441          3.2939
v  TurbVisc             6.8394e-14         0.14179      0.00041929       0.0063217
v  CourantNb             0.0003713           73975          64.504          16.418
v  FourierNb               0.22143      2.3653e+06          217.27          2.7541
v  total_pressure       4.9964e+05      5.1333e+05      5.0902e+05      5.0742e+05
v  Local Time Step            0.01         0.08456        0.010005        0.010038


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.1159      2.4393e+06          281.77          19.172


 TIME FOR THE TIME STEP              108:        0.19681E+03

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


 INSTANT    0.109000000E+02   TIME STEP NUMBER             109
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.69964a  k                   -9.4943e-05                            11
a  epsilon                 -2.1857                            37
a  Local Time Step      4.2278e-08                        281415


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.5857          3.3944         0.33687        0.079959
v  Velocity[Y]             -3.3422          4.8982         0.24104         0.19032
v  Velocity[Z]             -5.5862          3.8044        -0.17973     -0.00069252
v  ǁVelocityǁ             0.001088          6.2864          1.1192          1.5492
v  Pressure                -396.57           13601          9185.3            7541
v  k                    8.3121e-09         0.38412        0.003354       0.0076963
v  epsilon              3.1512e-06          6799.3          7.6236          3.3492
v  TurbVisc             7.0061e-14         0.14179      0.00042646       0.0063529
v  CourantNb             0.0055303           73124          65.535          16.543
v  FourierNb               0.22151      2.3653e+06          217.28          2.7552
v  total_pressure        4.996e+05       5.136e+05      5.0919e+05      5.0754e+05
v  Local Time Step            0.01        0.093016        0.010005        0.010037


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2916      2.4384e+06          282.81          19.299


 TIME FOR THE TIME STEP              109:        0.19209E+03

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


 INSTANT    0.110000000E+02   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        -0.389277714E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outa  k                   -9.4943e-05                            11
a  epsilon                 -2.1857                            37
a  Local Time Step      4.2278e-08                        281415


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.5857          3.3944         0.33687        0.079959
v  Velocity[Y]             -3.3422          4.8982         0.24104         0.19032
v  Velocity[Z]             -5.5862          3.8044        -0.17973     -0.00069252
v  ǁVelocityǁ             0.001088          6.2864          1.1192          1.5492
v  Pressure                -396.57           13601          9185.3            7541
v  k                    8.3121e-09         0.38412        0.003354       0.0076963
v  epsilon              3.1512e-06          6799.3          7.6236          3.3492
v  TurbVisc             7.0061e-14         0.14179      0.00042646       0.0063529
v  CourantNb             0.0055303           73124          65.535          16.543
v  FourierNb               0.22151      2.3653e+06          217.28          2.7552
v  total_pressure        4.996e+05       5.136e+05      5.0919e+05      5.0754e+05
v  Local Time Step            0.01        0.093016        0.010005        0.010037


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2916      2.4384e+06          282.81          19.299


 TIME FOR THE TIME STEP              109:        0.19523E+03

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


 INSTANT    0.110000000E+02   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        -0.389277714E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640682E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12301E+01 0.16236E+01
   Friction velocity        uet   :  0.11521E-01 0.34289E+02
   Friction velocity        uk    :  0.11519E-01 0.34289E+02
   Dimensionless distance   yplus :  0.43753E-02 0.90850E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2406
   Nb of faces within the viscous sub-layer     :      30245
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42147E+00     411   0.14385E+00   0.20123E+00 0.27533E+01 
c  Velocity[X]                                      0.41495E-01 
c  Velocity[Y]                                      0.89388E-01 
c  Velocity[Z]                                      0.70351E-01 
c  Pressure     0.41390E-01    1372   0.66656E-01   0.11744E+00 0.12477E+01 
c  k            0.14988E-01     166   0.52502E-03   0.72751E-04 0.55965E+01 
c  epsilon      0.13827E+03     188   0.65346E-03   0.40543E+04 0.25235E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.2529e-05                            14
a  epsilon                -0.14789                            12
a  Local Time Step      4.2278e-08                        281438


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -1.544          3.4342         0.33963        0.079911
v  Velocity[Y]             -3.3307          5.4602         0.24071         0.19039
v  Velocity[Z]             -5.6248          3.7076        -0.18414      -0.0010221
v  ǁVelocityǁ           0.00027548          6.3265           1.134           1.554
v  Pressure                -463.49           13803          9294.5         Dimensionless distance   yplus :  0.42928E-02 0.90373E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2437
   Nb of faces within the viscous sub-layer     :      30124
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42210E+00     411   0.14425E+00   0.18585E+00 0.26396E+01 
c  Velocity[X]                                      0.40754E-01 
c  Velocity[Y]                                      0.81719E-01 
c  Velocity[Z]                                      0.63377E-01 
c  Pressure     0.38297E-01    1322   0.59114E-01   0.10552E+00 0.10186E+01 
c  k            0.14896E-01     177   0.53019E-03   0.66310E-04 0.53322E+01 
c  epsilon      0.11716E+03     147   0.79639E-03   0.60069E+04 0.31471E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.2033e-05                             9
a  epsilon                 -2.1778                            26
a  Local Time Step      4.2278e-08                        281466


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.6571          3.4703         0.34184        0.079813
v  Velocity[Y]             -3.3512          5.4152         0.24084         0.19025
v  Velocity[Z]             -5.6441          3.6409        -0.18739      -0.0013577
v  ǁVelocityǁ           0.00037359          6.3432          1.1465          1.5578
v  Pressure                -523.37           13971          9381.7          7688.8
v  k                    7.7923e-09          0.3287       0.0035518       0.0077641
v  epsilon              1.1836e-05          6292.9          8.3522          3.4454
v  TurbVisc             6.3149e-   Dimensionless distance   yplus :  0.42928E-02 0.90373E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2437
   Nb of faces within the viscous sub-layer     :      30124
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42210E+00     411   0.14425E+00   0.18585E+00 0.26396E+01 
c  Velocity[X]                                      0.40754E-01 
c  Velocity[Y]                                      0.81719E-01 
c  Velocity[Z]                                      0.63377E-01 
c  Pressure     0.38297E-01    1322   0.59114E-01   0.10552E+00 0.10186E+01 
c  k            0.14896E-01     177   0.53019E-03   0.66310E-04 0.53322E+01 
c  epsilon      0.11716E+03     147   0.79639E-03   0.60069E+04 0.31471E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.2033e-05                             9
a  epsilon                 -2.1778                            26
a  Local Time Step      4.2278e-08                        281466


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.6571          3.4703         0.34184        0.079813
v  Velocity[Y]             -3.3512          5.4152         0.24084         0.19025
v  Velocity[Z]             -5.6441          3.6409        -0.18739      -0.0013577
v  ǁVelocityǁ           0.00037359          6.3432          1.1465          1.5578
v  Pressure                -523.37           13971          9381.7          7688.8
v  k                    7.7923e-09          0.3287       0.0035518       0.0077641
v  epsilon              1.1836e-05          6292.9          8.3522          3.4454
v  TurbVisc             6.3149e-14          0.1418       0.0004368       0.0063832
v  CourantNb              0.020511           69951           67.15          16.739
v  FourierNb               0.22162      2.3653e+06           217.3          2.7562
v  total_pressure       4.9948e+05      5.1397e+05      5.0938e+05      5.0769e+05
v  Local Time Step            0.01         0.11255        0.010005        0.010033


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6038      2.4352e+06          284.45          19.496


 TIME FOR THE TIME STEP              111:        0.18559E+03

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


 INSTANT    0.112000000E+02   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        -0.100549899E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640681E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11986E+01 0.15254E+01
   Friction velocity        uet   :  0.12702E-01 0.31762E+02
   Friction velocity        uk    :  0.12655E-01 0.31762E+02
   Dimensionless distance   yplus :  0.40529E-02 0.90265E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2447
   Nb of faces within the viscous sub-layer     :      30024
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42266E+00     412   0.14916E+00   0.18006E+00 0.25933E+01 
c  Velocity[X]                                      0.35289E-01 
c  Velocity[Y]    INSTANT    0.113000000E+02   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        -0.257347404E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640690E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11678E+01 0.14641E+01
   Friction velocity        uet   :  0.11117E-01 0.29900E+02
   Friction velocity        uk    :  0.11117E-01 0.29900E+02
   Dimensionless distance   yplus :  0.38153E-02 0.89698E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2467
   Nb of face INSTANT    0.113000000E+02   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        -0.257347404E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640690E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00 INSTANT    0.113000000E+02   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        -0.257347404E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640690E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11678E+01 0.14641E+01
   Friction velocity        uet   :  0.11117E-01 0.29900E+02
   Friction velocity        uk    :  0.11117E-01 0.29900E+02
   Dimensionless distance   yplus :  0.38153E-02 0.89698E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2467
   Nb of faces within the viscous sub-layer     :      29924
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42288E+00     413   0.15062E+00   0.17539E+00 0.25552E+01 
c  Velocity[X]                                      0.37484E-01 
c  Velocity[Y]                                      0.77599E-01 
c  Velocity[Z]                                      0.60311E-01 
c  Pressure     0.34568E-01    1297   0.49341E-01   0.91045E-01 0.84373E+00 
c  k            0.14937E-01     180   0.52169E-03   0.53912E-04 0.47889E+01 
c  epsilon      0.10782E+03     120   0.70578E-03   0.26262E+04 0.20761E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -3.555e-05                             5
a  epsilon                -0.12391                             6
a  Local Time Step      4.2278e-08                        281541


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.7511          3.5709         0.34463        0.079493
v  Velocity[Y]             -3.4585          5.6109         0.24119         0.19008
v  Velocity[Z]             -5.6783          3.6972        -0.19234      -0.0013697
v  ǁVelocityǁ           0.00038609          6.3782          1.1666          1.5635
v  Pressure                -602.78           14272          9542.8          7823.6
v  k                    7.2418e-09         0.28019       0.0036711       0.0078127
v  epsilon              2.6199e-05          5172.4          8.7159          3.5306
v  TurbVisc             5.8669e-14          0.1418      0.00044573       0.0063955
v  CourantNb              0.018522           63507          68.185          16.885
v  FourierNb               0.22171      2.3653e+06          217.31          2.7567
v  total_pressure        4.994e+05      5.1427e+05      5.0954e+05      5.0782e+05
v  Local Time Step            0.01         0.13618        0.010005        0.010032


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.667      2.4288e+06           285.5          19.642


 TIME FOR THE TIME STEP              113:        0.17842E+03

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


 INSTANT    0.114000000E+02   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         0.303968886E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640678E+00
Free inlet               13           0         0.000000000E+00
Convective i-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8274          3.5679         0.34566         0.07963
v  Velocity[Y]             -3.4245          5.7394          0.2415          0.1902
v  Velocity[Z]             -5.6946          3.6526        -0.19339      -0.0012337
v  ǁVelocityǁ           6.0721e-05          6.3792          1.1745           1.566
v  Pressure                -641.64           14397          9613.2          7877.8
v  k                    7.6902e-09         0.29431       0.0037618       0.0078308
v  epsilon              5.4212e-05          5030.8          9.1618          3.5545
v  TurbVisc             5.5943e-14          0.1418      0.00044986        0.006399
v  CourantNb              0.019409           61166          68.612          16.943
v  FourierNb               0.22175      2.3653e+06          217.31          2.7574
v  total_pressure       4.9936e+05       5.144e+05      5.0961e+05      5.0788e+05
v  Local Time Step            0.01          0.1498        0.010005        0.010033


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6338      2.4249e+06          285.93            19.7


 TIME FOR THE TIME STEP              114:        0.17757E+03

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


 INSTANT    0.115000000E+02   TIME STEP NUMBER             115
 ============================================================= 




   ** BOUNDARY MASS FLOW IN-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8274          3.5679         0.34566         0.07963
v  Velocity[Y]             -3.4245          5.7394          0.2415          0.1902
v  Velocity[Z]             -5.6946          3.6526        -0.19339      -0.0012337
v  ǁVelocityǁ           6.0721e-05          6.3792          1.1745           1.566
v  Pressure                -641.64           14397          9613.2          7877.8
v  k                    7.6902e-09         0.29431       0.0037618       0.0078308
v  epsilon              5.4212e-05          5030.8          9.1618          3.5545
v  TurbVisc             5.5943e-14          0.1418      0.00044986        0.006399
v  CourantNb              0.019409           61166          68.612          16.943
v  Fourie-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8274          3.5679         0.34566         0.07963
v  Velocity[Y]             -3.4245          5.7394          0.2415          0.1902
v  Velocity[Z]             -5.6946          3.6526        -0.19339      -0.0012337
v  ǁVelocityǁ           6.0721e-05          6.3792          1.1745           1.566
v  Pressure                -641.64           14397          9613.2          7877.8
v  k                    7.6902e-09         0.29431       0.0037618       0.0078308
v  epsilon              5.4212e-05          5030.8          9.1618          3.5545
v  TurbVisc             5.5943e-14          0.1418      0.00044986        0.006399
v  CourantNb              0.019409           61166          68.612          16.943
v  FourierNb               0.22175      2.3653e+06          217.31          2.7574
v  total_pressure       4.9936e+05       5.144e+05      5.0961e+05      5.0788e+05
v  Local Time Step            0.01          0.1498        0.010005        0.010033


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6338      2.4249e+06          285.93            19.7


 TIME FOR THE TIME STEP              114:        0.18239E+03

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


 INSTANT    0.115000000E+02   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        -0.326482562E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640681E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11294E+01 0.14185E+01
   Friction velocity        uet   :  0.11310E-01 0.26642E+02
   Friction velocity        uk    :  0.11310E-01 0.26642E+02
   Dimensionless distance   yplus :  0.33996E-02 0.88931E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2491
   Nb of faces within the viscous sub-layer     :      29729
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42394E+00     412   0.14891E+00   0.16346E+00 0.24602E+01 
c  Velocity[X]                                      0.39027E-01 
c  Velocity[Y]                                      0.70982E-01 
c  Velocity[Z]                                      0.53449E-01 
c  Pressure     0.33070E-01    1268   0.44116E-01   0.84351E-01 0.59806E+00 
c  k            0.14942E-01     167   0.43846E-03   0.40430E-04 0.41354E+01 
c  epsilon      0.99867E+02     129   0.59323E-03   0.15704E+04 0.16216E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.1838e-08                             1
a  epsilon              -0.0022325                             1
a  Local Time Step      4.2278e-08                        281541


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8358          3.5718         0.34647        0.079854
v  Velocity[Y]             -3.4004           5.613         0.24196         0.19032
v  Velocity[Z]             -5.7394          3.6442        -0.19392       -0.001225
v  ǁVelocityǁ           0.00084187          6.4333           1.181          1.5679
v  Pressure                 -681.7           14507          9676.2          7923.7
v  k                    5.1906e-09         0.28746       0.0037858       0.0078544
v  epsilon              5.0248e-05          4786.1          9.0361          3.5863
v  TurbVisc              5.956e-14          0.1418      0.00045365        0.006402
v  CourantNb             0.0092601        ------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42428E+00     413   0.15049E+00   0.16218E+00 0.24481E+01 
c  Velocity[X]                                      0.39555E-01 
c  Velocity[Y]                                      0.67791E-01 
c  Velocity[Z]                                      0.54831E-01 
c  Pressure     0.32289E-01    1229   0.41266E-01   0.81374E-01 0.48607E+00 
c  k            0.14970E-01     165   0.35563E-03   0.38731E-04 0.40427E+01 
c  epsilon      0.10060E+03     146   0.63892E-03   0.24395E+04 0.19858E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.1578e-05                             6
a  epsilon                 -7.8184                            24
a  Local Time Step      4.2278e-08                        281527


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8336          3.5913         0.34706        0.------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42428E+00     413   0.15049E+00   0.16218E+00 0.24481E+01 
c  Velocity[X]                                      0.39555E-01 
c  Velocity[Y]                                      0.67791E-01 
c  Velocity[Z]                                      0.54831E-01 
c  Pressure     0.32289E-01    1229   0.41266E-01   0.81374E-01 0.48607E+00 
c  k            0.14970E-01     165   0.35563E-03   0.38731E-04 0.40427E+01 
c  epsilon      0.10060E+03     146   0.63892E-03  ------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42428E+00     413   0.15049E+00   0.16218E+00 0.24481E+01 
c  Velocity[X]                                      0.39555E-01 
c  Velocity[Y]                                      0.67791E-01 
c  Velocity[Z]                                      0.54831E-01 
c  Pressure     0.32289E-01    1229   0.41266E-01   0.81374E-01 0.48607E+00 
c  k            0.14970E-01     165   0.35563E-03   0.38731E-04 0.40427E+01 
c  epsilon      0.10060E+03     146   0.63892E-03   0.24395E+04 0.19858E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.1578e-05                             6
a  epsilon                 -7.8184                            24
a  Local Time Step      4.2278e-08                        281527


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8336          3.5913         0.34706        0.079982
v  Velocity[Y]             -3.3985          5.5374         0.24226         0.19033
v  Velocity[Z]             -5.7264          3.6351        -0.19342      -0.0011679
v  ǁVelocityǁ            0.0021348          6.3812          1.1859          1.5696
v  Pressure                -731.68           14597          9727.3          7959.7
v  k                    4.8857e-09         0.34284       0.0038342       0.0078693
v  epsilon              3.4872e-05          5104.8          9.3067          3.6147
v  TurbVisc             3.1276e-14          0.1418      0.00045709        0.006405
v  CourantNb             0.0091012           51716          69.194          17.028
v  FourierNb               0.22183      2.3653e+06          217.32           2.758
v  total_pressure       4.9927e+05       5.146e+05      5.0973e+05      5.0796e+05
v  Local Time Step            0.01         0.17316        0.010005        0.010032


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6202       2.417e+06          286.51          19.786


 TIME FOR THE TIME STEP              116:        0.17114E+03

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


 INSTANT    0.117000000E+02   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        -0.325394640E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640670E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10868E+01 0.13779E+01
   Friction velocity        uet   :  0.16644E-01 0.23312E+02
   Friction velocity        uk    :  0.16585E-01 0.23312E+02
   Dimensionless distance   yplus :  0.29746E-02 0.88095E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2491
   Nb of faces within the viscous sub-layer     :      29574
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42487E+00     412   0.15224E+00   0.16245E+00 0.24482E+01 
c  Velocity[X]                                      0.40429E-01 
c  Velocity[Y]                                      0.68229E-01 
c  Velocity[Z]                                      0.53795E-01 
c  Pressure     0.31333E-01    1231   0.38589E-01   0.78167E-01 0.41343E+00 
c  k            0.14905E-01     178   0.63560E-03   0.45928E-04 0.43961E+01 
c  Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.109942591E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640659E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ----------------------------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.109942591E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640659E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   -----------------------------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.109942591E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640659E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   -----------------------------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.109942591E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640659E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           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+01 0.14023E+01
   Friction velocity        uet   :  0.19147E-01 0.21310E+02
   Friction velocity        uk    :  0.19049E-01 0.21310E+02
   Dimensionless distance   yplus :  0.27191E-02 0.87458E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2498
   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     0.42523E+00     409   0.15161E+00   0.16279E+00 0.24487E+01 
c  Velocity[X]                                      0.40952E-01 
c  Velocity[Y]                                      0.68011E-01 
c  Velocity[Z]                                      0.53830E-01 
c  Pressure     0.30451E-01    1222   0.35899E-01   0.75346E-01 0.36660E+00 
c  k            0.14934E-01     168   0.50493E-03   0.42026E-04 0.42002E+01 
c  epsilon      0.86143E+02     128   0.72426E-03   0.22323E+04 0.19096E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00010642                            17
a  epsilon                 -2.1523                            22
a  Local Time Step      4.2278e-08                        281539


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8919          3.6056         0.34746        0.080118
v  Velocity[Y]             -3.4317          5.1462         0.24256         0.19023
v  Velocity[Z]             -5.7864          3.6117        -0.19301       -0.001081
v  ǁVelocityǁ            0.0028729          6.4274           1.194          1.5721
v  Pressure                -843.88           14734          9806.7          8018.2
v  k                    1.9719e-09         0.30796       0.0039357       0.0079063
v  epsilon              6.7864e-05          4796.1           9.571          3.6714
v  TurbVisc             5.3449e-14          0.1418       0.0004634       0.0064095
v  CourantNb             0.0052875           46712          69.546          17.085
v  FourierNb               0.22191      2.3653e+06          217.33          2.7589
v  total_pressure       4.9916e+05      5.1473e+05      5.0981e+05      5.0802e+05
v  Local Time Step            0.01        0.076133        0.010005        0.010027


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6488       2.412e+06          286.88          19.843


 TIME FOR THE TIME STEP              118:        0.18486E+03

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


 INSTANT    0.119000000E+02   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        -0.677917977E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640670E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   v  Velocity[Z]             -6.2748          3.6208         -0.1926      -0.0010357
v  ǁVelocityǁ           0.00043442          6.8282          1.1972          1.5731
v  Pressure                -901.79           14782          9833.3          8041.2
v  k                     4.112e-09         0.37377       0.0039734       0.0079245
v  epsilon              7.5334e-05          5742.2          9.6963          3.7076
v  TurbVisc             9.2468e-15          0.1418      0.00046578       0.0064113
v  CourantNb              0.013891           41871          69.667          17.106
v  FourierNb               0.22197      2.3653e+06          217.33          2.7588
v  total_pressure        4.991e+05      5.1478e+05      5.0983e+05      5.0804e+05
v  Local Time Step            0.01         0.07228        0.010004        0.010025


  ** Cv  Velocity[Z]             -6.2748          3.6208         -0.1926      -0.0010357
v  ǁVelocityǁ           0.00043442          6.8282          1.1972          1.5731
v  Pressure                -901.79           14782          9833.3          8041.2
v  k                     4.112e-09         0.37377       0.0039734       0.0079245
v  epsilon              7.5334e-05          5742.2          9.6963          3.7076
v  TurbVisc             9.2468e-15          0.1418      0.00046578       0.0064113
v  CourantNb              0.013891           41871          69.667          17.106
v  FourierNb               0.22197      2.3653e+06          217.33          2.7588
v  total_pressure        4.991e+05      5.1478e+05      5.0983e+05      5.0804e+05
v  Local Time Step            0.01         0.07228        0.010004        0.010025


  ** Cov  Velocity[Z]             -6.2748          3.6208         -0.1926      -0.0010357
v  ǁVelocityǁ           0.00043442          6.8282          1.1972          1.5731
v  Pressure                -901.79           14782          9833.3          8041.2
v  k                     4.112e-09         0.37377       0.0039734       0.0079245
v  epsilon              7.5334e-05          5742.2          9.6963          3.7076
v  TurbVisc             9.2468e-15          0.1418      0.00046578       0.0064113
v  CourantNb              0.013891           41871          69.667          17.106
v  FourierNb               0.22197      2.3653e+06          217.33          2.7588
v  total_pressure        4.991e+05      5.1478e+05      5.0983e+05      5.0804e+05
v  Local Time Step            0.01         0.07228        0.010004        0.010025


  ** Cov  Velocity[Z]             -6.2748          3.6208         -0.1926      -0.0010357
v  ǁVelocityǁ           0.00043442          6.8282          1.1972          1.5731
v  Pressure                -901.79           14782          9833.3          8041.2
v  k                     4.112e-09         0.37377       0.0039734       0.0079245
v  epsilon              7.5334e-05          5742.2          9.6963          3.7076
v  TurbVisc             9.2468e-15          0.1418      0.00046578       0.0064113
v  CourantNb              0.013891           41871          69.667          17.106
v  FourierNb               0.22197      2.3653e+06          217.33          2.7588
v  total_pressure        4.991e+05      5.1478e+05      5.0983e+05      5.0804e+05
v  Local Time Step            0.01         0.07228        0.010004        0.010025


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6748      2.4072e+06             287          19.865


 TIME FOR THE TIME STEP              119:        0.16993E+03

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


 INSTANT    0.120000000E+02   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        -0.732944537E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640659E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           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+01 0.13643E+01
   Friction velocity        uet   :  0.91591E-02 0.17317E+02
   Friction velocity        uk    :  0.91582E-02 0.17317E+02
   Dimensionless distance   yplus :  0.22097E-02 0.88323E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2517
   Nb of faces within the viscous sub-layer     :      29343
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42584E+00     405   0.15751E+00   0.14410E+00 0.23007E+01 
c  Velocity[X]                                      0.37075E-01 
c  Velocity[Y]                                      0.61057E-01 
c  Velocity[Z]                                      0.45970E-01 
c  Pressure     0.27356E-01    1084   0.30072E-01   0.66772E-01 0.23774E+00 
c  k            0.14999E-01     176   0.31438E-03   0.29707E-04 0.35235E+01 
c  epsilon      0.86200E+02     123   0.37955E-03   0.91433E+03 0.12094E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00031448                            10
a  epsilon                 -4.8447                            28
a  Local Time Step      4.2278e-08                        281550


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -1.911            3.62          0.3479        0.080119
v  Velocity[Y]             -3.4396          4.9859         0.24477          0.1901
v  Velocity[Z]             -5.9034          3.5937        -0.19234     -0.00099743
v  ǁVelocityǁ           0.00045555          6.5277          1.2004          1.5741
v  Pressure                -959.72           14816          9850.4          8058.1
v  k                    5.5207e-09         0.34727       0.0040073       0.0079359
v  epsilon              7.3016e-05          5163.1           9.778          3.7224
v  TurbVisc             3.9993e-14          0.1418      0.00046949       0.0064129
v  CourantNb              0.025431           38821          69.769          17.123
v  FourierNb               0.22202      2.3653e+06          217.34          2.7594
v  total_pressure       4.9904e+05      5.1482e+05      5.0985e+05      5.0806e+05
v  Local Time Step            0.01        0.079508        0.010004        0.010-----------------------------------------------------------------------------
c  Velocity     0.42592E+00     402   0.15576E+00   0.13818E+00 0.22519E+01 
c  Velocity[X]                                      0.36826E-01 
c  Velocity[Y]                                      0.58677E-01 
c  Velocity[Z]                                      0.42681E-01 
c  Pressure     0.26145E-01     938   0.27666E-01   0.63419E-01 0.14839E+00 
c  k            0.15028E-01     169   0.27702E-03   0.21938E-04 0.30248E+01 
c  epsilon      0.86726E+02     139   0.40068E-03   0.77883E+03 0.11061E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  ---------------------------------------------------------------------------------
c  Velocity     0.42592E+00     402   0.15576E+00   0.13818E+00 0.22519E+01 
c  Velocity[X]                                      0.36826E-01 
c  Velocity[Y]                                      0.58677E-01 
c  Velocity[Z]                                      0.42681E-01 
c  Pressure     0.26145E-01     938   0.27666E-01   0.63419E-01 0.14839E+00 
c  k            0.15028E-01     169   0.27702E-03   0.21938E-04 0.30248E+01 
c  epsilon      0.86726E+02     139   0.40068E-03   0.77883E+03 0.11061E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  ----------------------------------------------------------------------------------
c  Velocity     0.42592E+00     402   0.15576E+00   0.13818E+00 0.22519E+01 
c  Velocity[X]                                      0.36826E-01 
c  Velocity[Y]                                      0.58677E-01 
c  Velocity[Z]                                      0.42681E-01 
c  Pressure     0.26145E-01     938   0.27666E-01   0.63419E-01 0.14839E+00 
c  k            0.15028E-01     169   0.27702E-03   0.21938E-04 0.30248E+01 
c  epsilon      0.86726E+02     139   0.40068E-03   0.77883E+03 0.11061E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  ----------------------------------------------------------------------------------
c  Velocity     0.42592E+00     402   0.15576E+00   0.13818E+00 0.22519E+01 
c  Velocity[X]                                      0.36826E-01 
c  Velocity[Y]                                      0.58677E-01 
c  Velocity[Z]                                      0.42681E-01 
c  Pressure     0.26145E-01     938   0.27666E-01   0.63419E-01 0.14839E+00 
c  k            0.15028E-01     169   0.27702E-03   0.21938E-04 0.30248E+01 
c  epsilon      0.86726E+02     139   0.40068E-03   0.77883E+03 0.11061E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.7986e-05                             1
a  epsilon        
a  Local Time Step      4.2278e-08                        281547


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9326           3.604         0.34807        0.080264
v  Velocity[Y]             -3.4861            4.86         0.24563         0.19009
v  Velocity[Z]             -5.9397          3.6199        -0.19244     -0.00097461
v  ǁVelocityǁ           0.00065318           6.622          1.2033          1.5751
v  Pressure                -1013.7           14834          9854.2          8066.3
v  k                    5.1911e-09         0.35992       0.0040367       0.0079478
v  epsilon              7.3567e-05          5700.4          9.8913          3.7449
v  TurbVisc             3.9376e-14          0.1418      0.00047217       0.0064138
v  CourantNb              0.024807           39037          69.904          17.141
v  FourierNb               0.22208      2.3653e+06          217.34          2.7597
v  total_pressure       4.9899e+05      5.1483e+05      5.0985e+05      5.0807e+05
v  Local Time Step            0.01        0.087459        0.010004        0.010024


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6614      2.4016e+06          287.25          19.901


 TIME FOR THE TIME STEP              121:        0.17200E+03

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


 INSTANT    0.122000000E+02   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        -0.475668510E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640655E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11515E+01 0.13668E+01
   Friction velocity        uet   :  0.14611E-01 0.14364E+02
   Friction velocity        uk    :  0.14609E-01 0.14364E+02
   Dimensionless distance   yplus :  0.18247E-02 0.89073E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2514
   Nb of faces within the viscous sub-layer     :      29230
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42602E+00     400   0.15487E+00   0.13668E+00 0.22380E+01 
c  Velocity[X]                                      0.35276E-01 
c  Velocity[Y]                                      0.59965E-01 
c  Velocity[Z]                                      0.41440E-01 
c  Pressure     0.24775E-01     973   0.25849E-01   0.59759E-01 0.94553E-01 
c  k            0.15037E-01     166   0.30463E-03   0.28327E-04 0.34347E+01 
c  epsilon      0.85814E+02     110   0.32488E-03   0.84834E+03 0.11528E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ----Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11781E+01 0.13660E+01
   Friction velocity        uet   :  0.75314E-02 0.14420E+02Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11781E+01 0.13660E+01
   Friction velocity        uet   :  0.75314E-02 0.14420E+02
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11781E+01 0.13660E+01
   Friction velocity        uet   :  0.75314E-02 0.14420E+02
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640972E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11781E+01 0.13660E+01
   Friction velocity        uet   :  0.75314E-02 0.14420E+02
   Friction velocity        uk    :  0.75260E-02 0.14420E+02
   Dimensionless distance   yplus :  0.16213E-02 0.89518E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2524
   Nb of faces within the viscous sub-layer     :      29177
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42618E+00     399   0.15707E+00   0.13853E+00 0.22521E+01 
c  Velocity[X]                                      0.32967E-01 
c  Velocity[Y]                                      0.60948E-01 
c  Velocity[Z]                                      0.44615E-01 
c  Pressure     0.23433E-01    1098   0.24270E-01   0.56209E-01 0.11756E+00 
c  k            0.15034E-01     154   0.41640E-03   0.33974E-04 0.37597E+01 
c  epsilon      0.84371E+02     101   0.55985E-03   0.16895E+04 0.16339E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.4492e-05                            11
a  epsilon               -0.056878                             7
a  Local Time Step      4.2278e-08                        281560


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9525          3.6155         0.34927        0.080431
v  Velocity[Y]             -3.4808          4.7063         0.24645         0.19006
v  Velocity[Z]             -5.9734          3.6079        -0.19298       -0.001022
v  ǁVelocityǁ           0.00059553          6.6231          1.2078          1.5766
v  Pressure                -1096.6           14832            9830          8058.9
v  k                    4.4597e-09         0.36256       0.0040897        0.007965
v  epsilon               9.052e-05            5527          10.032          3.7734
v  TurbVisc             3.7146e-14          0.1418      0.00047637       0.0064155
v  CourantNb              0.019926           41000          70.176          17.169
v  FourierNb               0.22216      2.3653e+06          217.35          2.7597
v  total_pressure        4.989e+05      5.1483e+05      5.0983e+05      5.0806e+05
v  Local Time Step            0.01         0.10582        0.010004        0.010022


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6449      2.3986e+06          287.52          19.928


 TIME FOR THE TIME STEP              123:        0.16599E+03

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


 INSTANT    0.124000000E+02   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        -0.421673322E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699641002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11886E+01 0.13685E+01
   Fricv  epsilon              0.00011939          5293.6          10.067          3.7925
v  TurbVisc             3.1358e-14          0.1418      0.00047866        0.006416
v  CourantNb              0.022079           42569          70.309          17.177
v  FourierNb               0.22218      2.3653e+06          217.35          2.7599
v  total_pressure       4.9888e+05      5.1482e+05      5.0981e+05      5.0805e+05
v  Local Time Step            0.01         0.11641        0.010004        0.010021


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6198      2.3994e+06          287.66          19.937


 TIME FOR THE TIME STEP     v  epsilon              0.00011939          5293.6          10.067          3.7925
v  TurbVisc             3.1358e-14          0.1418      0.00047866        0.006416
v  CourantNb              0.022079           42569          70.309          17.177
v  FourierNb               0.22218      2.3653e+06          217.35          2.7599
v  total_pressure       4.9888e+05      5.1482e+05      5.0981e+05      5.0805e+05
v  Local Time Step            0.01         0.11641        0.010004        0.010021


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6198      2.3994e+06          287.66          19.937


 TIME FOR THE TIME STEP      v  epsilon              0.00011939          5293.6          10.067          3.7925
v  TurbVisc             3.1358e-14          0.1418      0.00047866        0.006416
v  CourantNb              0.022079           42569          70.309          17.177
v  FourierNb               0.22218      2.3653e+06          217.35          2.7599
v  total_pressure       4.9888e+05      5.1482e+05      5.0981e+05      5.0805e+05
v  Local Time Step            0.01         0.11641        0.010004        0.010021


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6198      2.3994e+06          287.66          19.937


 TIME FOR THE TIME STEP      v  epsilon              0.00011939          5293.6          10.067          3.7925
v  TurbVisc             3.1358e-14          0.1418      0.00047866        0.006416
v  CourantNb              0.022079           42569          70.309          17.177
v  FourierNb               0.22218      2.3653e+06          217.35          2.7599
v  total_pressure       4.9888e+05      5.1482e+05      5.0981e+05      5.0805e+05
v  Local Time Step            0.01         0.11641        0.010004        0.010021


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6198      2.3994e+06          287.66          19.937


 TIME FOR THE TIME STEP              124:        0.16971E+03

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


 INSTANT    0.125000000E+02   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        -0.588810020E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699641030E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12014E+01 0.13687E+01
   Friction velocity        uet   :  0.20945E-01 0.14816E+02
   Friction velocity        uk    :  0.20909E-01 0.14816E+02
   Dimensionless distance   yplus :  0.14858E-02 0.89926E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2528
   Nb of faces within the viscous sub-layer     :      29091
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42641E+00     395   0.15909E+00   0.15912E+00 0.24114E+01 
c  Velocity[X]                                      0.38796E-01 
c  Velocity[Y]                                      0.71158E-01 
c  Velocity[Z]                                      0.49167E-01 
c  Pressure     0.23948E-01    1065   0.24484E-01   0.56978E-01 0.11884E+00 
c  k            0.15063E-01     151   0.37297E-03   0.31322E-04 0.36048E+01 
c  epsilon      0.83077E+02     126   0.61695E-03   0.11930E+04 0.13618E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00031589                             9
a  epsilon                -0.87112                             5
a  Local Time Step      4.2278e-08                        281558


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9409          3.5826         0.35145        0.080368
v  Velocity[Y]             -3.5152           4.639         0.24713         0.19017
v  Velocity[Z]              -5.901          3.6178        -0.19548      -0.0010536
v  ǁVelocityǁ           0.00093751          6.5829          1.2129          1.5777
v  Pressure                -1115.2           14813          9795.3          8040.8
v  k                    5.0221e-09         0.35972       0.0041536       0.0079772
v  epsilon              0.00010412          5457.9          10.269          3.8068
v  TurbVisc             3.7381e-14          0.1418      0.00048075       0.0064166
v  CourantNb             0.0074768           43936          70.526          17.191
v  FourierNb               0.22218      2.3653e+06          217.36          2.7602
v  total_pressure       4.9888e+05      5.1481e+05       5.098e+05      5.0804e+05
v  Local Time Step            0.01         0.12805        0.010004        0.010021


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6164      2.3988e+06  c  Velocity[Z]                                      0.52312E-01 
c  Pressure     0.24295E-01    1029   0.25295E-01   0.57644E-01 0.10295E+00 
c  k            0.15086E-01     155   0.31439E-03   0.21791E-04 0.30061E+01 
c  epsilon      0.85370E+02     250   0.43121E-03   0.77319E+03 0.10960E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.8753e-05                             6
a  epsilon                  -2.139                            24
a  Local Time Step      4.2278e-08                        281552


  ** Computed fields on cells
   c  Velocity[Z]                                      0.52312E-01 
c  Pressure     0.24295E-01    1029   0.25295E-01   0.57644E-01 0.10295E+00 
c  k            0.15086E-01     155   0.31439E-03   0.21791E-04 0.30061E+01 
c  epsilon      0.85370E+02     250   0.43121E-03   0.77319E+03 0.10960E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.8753e-05                             6
a  epsilon                  -2.139                            24
a  Local Time Step      4.2278e-08                        281552


  ** Computed fields on cells
    c  Velocity[Z]                                      0.52312E-01 
c  Pressure     0.24295E-01    1029   0.25295E-01   0.57644E-01 0.10295E+00 
c  k            0.15086E-01     155   0.31439E-03   0.21791E-04 0.30061E+01 
c  epsilon      0.85370E+02     250   0.43121E-03   0.77319E+03 0.10960E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.8753e-05                             6
a  epsilon                  -2.139                            24
a  Local Time Step      4.2278e-08                        281552


  ** Computed fields on cells
    c  Velocity[Z]                                      0.52312E-01 
c  Pressure     0.24295E-01    1029   0.25295E-01   0.57644E-01 0.10295E+00 
c  k            0.15086E-01     155   0.31439E-03   0.21791E-04 0.30061E+01 
c  epsilon      0.85370E+02     250   0.43121E-03   0.77319E+03 0.10960E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.8753e-05                             6
a  epsilon                  -2.139                            24
a  Local Time Step      4.2278e-08                        281552


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9443          3.6041         0.35279        0.080365
v  Velocity[Y]             -3.5075           4.686         0.24739         0.19027
v  Velocity[Z]             -6.0784          3.5903        -0.19732      -0.0010637
v  ǁVelocityǁ           0.00071352          6.7491          1.2159          1.5784
v  Pressure                -1094.1           14808          9785.3          8034.8
v  k                    5.1382e-09         0.35377       0.0041584       0.0079804
v  epsilon              0.00012921          5340.4          10.199          3.8155
v  TurbVisc             3.7701e-14          0.1418      0.00048221       0.0064167
v  CourantNb            0.00064191           46331          70.638          17.198
v  FourierNb               0.22216      2.3653e+06          217.36          2.7595
v  total_pressure       4.9891e+05      5.1481e+05      5.0979e+05      5.0803e+05
v  Local Time Step            0.01         0.14085        0.010004        0.010021


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6134      2.3959e+06             288          19.958


 TIME FOR THE TIME STEP              126:        0.20473E+03

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


 INSTANT    0.127000000E+02   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        -0.805549211E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699641026E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12092E+01 0.13795E+01
   Friction velocity        uet   :  0.12935E-01 0.15502E+02
   Friction velocity        uk    :  0.12817E-01 0.15502E+02
   Dimensionless distance   yplus :  0.19589E-02 0.90065E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2531
   Nb of faces within the viscous sub-layer     :      29039
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42613E+00     385   0.15903E+00   0.16519E+00 0.24546E+01 
c  Velocity[X]                                      0.40532E-01 
c  Velocity[Y]                                      0.69107E-01 
c  Velocity[Z]                                      0.55550E-01 
c  Pressure     0.25909E-01     723   0.26475E-01   0.61379E-01 0.83397E-01 
c  k            0.15107E-01     153   0.33199E-03   0.21406E-04 0.29776E+01 
c  epsilon      0.84187E+02     136   0.47615E-03   0.73983E+03 0.10651E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -3.248e-05                             7
a  epsilon                -0.12056                            13
a  Local Time Step      4.2278e-08                    Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12074E+01 0.13795E+01
   Friction velocity        uet   :  0.82093E-02 0.15411E+02
   Friction velocity        uk    :  0.86397E-02 0.15411E+02
   Dimensionless distance   yplus :  0.19665E-02 0.90048E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2541
   Nb of faces within the viscous sub-layer     :      29035
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42628E+00     382   0.15512E+00   0.15555E+00 0.23809E+01 
c  Velocity[X]                                      0.39495E-01 
c  Velocity[Y]                                      0.62290E-01 
c  Velocity[Z]                                      0.53761E-01 
c  Pressure     0.25613E-01    1046   0.26206E-01   0.60635E-01 0.11133E+00 
c  k            0.15130E-01     151   0.29704E-03   0.23119E-04 0.30930E+01 
c  epsilon      0.85130E+02     156   0.37988E-03   0.67049E+03 0.10110E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00015568                             8
a  epsilon                 -2.0952                            30
a  Local Time Step      4.2278e-08                        281570


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12074E+01 0.13795E+01
   Friction velocity        uet   :  0.82093E-02 0.15411E+02
   Friction velocity        uk    :  0.86397E-02 0.15411E+02
   Dimensionless distance   yplus :  0.19665E-02 0.90048E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2541
   Nb of faces within the viscous sub-layer     :      29035
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42628E+00     382   0.15512E+00   0.15555E+00 0.23809E+01 
c  Velocity[X]                                      0.39495E-01 
c  Velocity[Y]                                      0.62290E-01 
c  Velocity[Z]                                      0.53761E-01 
c  Pressure     0.25613E-01    1046   0.26206E-01   0.60635E-01 0.11133E+00 
c  k            0.15130E-01     151   0.29704E-03   0.23119E-04 0.30930E+01 
c  epsilon      0.85130E+02     156   0.37988E-03   0.67049E+03 0.10110E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00015568                             8
a  epsilon                 -2.0952                            30
a  Local Time Step      4.2278e-08                        281570


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8581          3.5384         0.35385         0.08045
v  Velocity[Y]             -3.4933          4.7018         0.24822         0.19063
v  Velocity[Z]             -5.9153          3.5977        -0.20058      -0.0010262
v  ǁVelocityǁ           0.00041022          6.6105          1.2207          1.5787
v  Pressure                -1019.5           14829            9795          8041.6
v  k                    5.2687e-09          0.3526        0.004194       0.0079896
v  epsilon              0.00013414            5306          10.341          3.8402
v  TurbVisc             3.9597e-14          0.1418      0.00048434       0.0064173
v  CourantNb              0.011061           47060           71.06          17.217
v  FourierNb               0.22214      2.3653e+06          217.36            2.76
v  total_pressure       4.9898e+05      5.1483e+05       5.098e+05      5.0804e+05
v  Local Time Step            0.01         0.15414        0.010004         0.01002


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.583      2.3926e+06          288.42          19.977


 TIME FOR THE TIME STEP              128:        0.21118E+03

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


 INSTANT    0.129000000E+02   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        -0.881718223E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640652E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12210E+01 0.14050E+01
   Friction velocity        uet   :  0.15386E-01 0.15572E+02
   Friction velocity        uk    :  0.15332E-01 0.15572E+02
   Dimensionless distance   yplus :  0.19870E-02 0.90287E+01
   ------------------------------------------------------
   Nb of reversv  FourierNb               0.22213      2.3653e+06          217.37          2.7602
v  total_pressure       4.9902e+05      5.1484e+05      5.0981e+05      5.0805e+05
v  Local Time Step            0.01         0.16587        0.010004         0.01002


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5728      2.3932e+06          288.58          19.981


 TIME FOR THE TIME STEP              129:        0.22341E+03

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


 INSTANT    0.130000000E+02   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        -0.570178267E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640659E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12447E+01 0.13997E+01
   Friction velocity        uet   :  0.17869E-01 0.15163E+02
   Friction velocity        uk    :  0.17650E-01 0.15163E+02
   Dimensionless distance   yplus :  0.19348E-02 0.90685E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2531
   Nb of faces within the viscous sub-layer     :      29004
   Total number of wall faces                   :      41000
-----------------------------------------v  FourierNb               0.22213      2.3653e+06          217.37          2.7602
v  total_pressure       4.9902e+05      5.1484e+05      5.0981e+05      5.0805e+05
v  Local Time Step            0.01         0.16587        0.010004         0.01002


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5728      2.3932e+06          288.58          19.981


 TIME FOR THE TIME STEP              129:        0.21786E+03

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


 INSTANT    0.130000000E+02   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        -0.570178267E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640659E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12447E+01 0.13997E+01
   Friction velocity        uet   :  0.17869E-01 0.15163E+02
   Friction velocity        uk    :  0.17650E-01 0.15163E+02
   Dimensionless distance   yplus :  0.19348E-02 0.90685E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2531
   Nb of faces within the viscous sub-layer     :      29004
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42702E+00     378   0.16403E+00   0.13437E+00 0.22118E+01 
c  Velocity[X]                                      0.32930E-01 
c  Velocity[Y]                                      0.51950E-01 
c  Velocity[Z]                                      0.49491E-01 
c  Pressure     0.24454E-01    1013   0.23627E-01   0.57815E-01 0.11471E+00 
c  k            0.15161E-01     154   0.22083E-03   0.14627E-04 0.24586E+01 
c  epsilon      0.86637E+02     142   0.32970E-03   0.39511E+03 0.77344E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.0008e-05                             4
a  epsilon               -0.013064                             5
a  Local Time Step      4.2278e-08                        281572


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.7615          3.4927         0.35408        0.080717
v  Velocity[Y]             -3.5024          4.9115         0.24903         0.19115
v  Velocity[Z]             -6.1115          3.5908         -0.2022     -0.00083945
v  ǁVelocityǁ           0.00044756          6.8089          1.2229          1.5788
v  Pressure                -955.12           14859          9818.3          8055.7
v  k                    5.6183e-09          0.3564       0.0042181       0.0079968
v  epsilon              0.00013183          5396.5          10.458          3.8531
v  TurbVisc             4.0514e-14          0.1418      0.00048567        0.006418
v  CourantNb             0.0029132           46642          71.223           17.22
v  FourierNb               0.22214      2.3653e+06          217.37          2.7601
v  total_pressure       4.9904e+05      5.1486e+05      5.0982e+05      5.0806e+05
v  Local Time Step            0.01         0.11484        0.010004        0.010017


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5536      2.3916e+06          288.59           19.98


 TIME FOR THE TIME STEP              130:        0.21227E+03

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


 INSTANT    0.131000000E+02   TIME STEP NUMBER             131
 ============================================================= 




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

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00013316                            36
a  epsilon                 -2.1959                            69
a  Local Time Step      4.2278e-08                        281571


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.7746          3.5342         0.35371        0.080806
v  Velocity[Y]             -3.5135          4.9121         0.24933         0.19109
v  Velocity[Z]             -6.0392          3.5828        -0.20257     -0.00077624
v  ǁVelocityǁ           0.00034419          6.7292          1.2233          1.5787
v  Pressure                -941.38           14867          9823.9          8058.2
v  k                     5.775e-09         0.36077       0.0042339       0.0080021
v  epsilon              5.7158e-05          5498.2          10.481          3.8595
v  TurbVisc             4.2548e-14          0.1418      0.00048639       0.0064185
v  CourantNb            0.00059835           46857          71.268          17.221
v  FourierNb               0.22215      2.3653e+06          217.37          2.7599
v  total_pressure       4.9906e+05      5.1487e+05      5.0982e+05      5.0806e+05
v  Local Time Step            0.01        0.093044        0.010004        0.010016


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5356      2.3909e+06          288.64          19.981


 TIME FOR THE TIME STEP              131:        0.21843E+03

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


 INSTANT    0.132000000E+02   TIME STEP NUMBER             132
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
-------------------------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00013316                            36
a  epsilon                 -2.1959                            69
a  Local Time Step      4.2278e-08                        281571


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.7746          3.5342         0.35371        0.080806
v  Velocity[Y]             -3.5135          4.9121         0.24933         0.19109
v  Velocity[Z]             -6.0392          3.5828        -0.20257     -0.00077624
v  ǁVelocityǁ           0.00034419          6.7292          1.2233          1.5787
v  Pressure                -941.38           14867          9823.9          8058.2
v  k                     5.775e-09         0.36077       0.0042339       0.0080021
v  epsilon              5.7158e-05          5498.2          10.481          3.8595
v  TurbVisc             4.2548e-14          0.1418      0.00048639       0.0064185
v  CourantNb            0.00059835           46857          71.268          17.221
v  FourierNb               0.22215      2.3653e+06          217.37          2.7599
v  total_pressure       4.9906e+05      5.1487e+05      5.0982e+05      5.0806e+05
v  Local Time Step            0.01        0.093044        0.010004        0.010016


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5356      2.3909e+06          288.64          19.981


 TIME FOR THE TIME STEP              131:        0.21181E+03

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


 INSTANT    0.132000000E+02   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        -0.437255324E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640654E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13024E+01 0.14102E+01
   Friction velocity        uet   :  0.13788E-01 0.17317E+02
   Friction velocity        uk    :  0.13656E-01 0.17317E+02
   Dimensionless distance   yplus :  0.22097E-02 0.91614E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2528
   Nb of faces within the viscous sub-layer     :      28975
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42696E+00     371   0.16067E+00   0.12552E+00 0.21372E+01 
c  Velocity[X]                                      0.31301E-01 
c  Velocity[Y]                                      0.49184E-01 
c  Velocity[Z]                                      0.45031E-01 
c  Pressure     0.23617E-01     922   0.22438E-01   0.55765E-01 0.65568E-01 
c  k            0.15168E-01     142   0.28632E-03   0.22192E-04 0.30260E+01 
c  epsilon      0.87386E+02     166   0.37147E-03   0.82874E+03 0.11150E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.1951e-05                             5
a  epsilon               -0.037084                            19
a  Local Time Step      4.2278e-08                        281551


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8134      ------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13319E+01 0.14050E+01
   Friction velocity        uet   :  0.20280E-01 0.17432E+02
   Friction velocity        uk    :  0.20060E-01 0.17432E+02
   Dimensionless distance   yplus :  0.22244E-02 0.92086E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2520
   Nb of faces within the viscous sub-layer     :      28955
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42702E+00     374   0.15787E+00   0.12096E+00 0.20975E+01 
c  Velocity[X]                                      0.29319E-01 
c  Velocity[Y]                                      0.46700E-01 
c  Velocity[Z]                                      0.44937E-01 
c  Pressure     0.22470E-01     919   0.21125E-01   0.52995E-01 0.65420E-01 
c  k            0.15177E-01     163   0.25103E-03   0.22107E-04 0.30184E+01 
c  epsilon      0.86815E+02     132   0.37125E-03   0.61932E+03 0.96462E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.4592e-05                             6
a  epsilon              -0.0071955                             9
a  Local Time Step      4.2278e-08                        281552


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8844          3.5181         0.35385        0.080856
v  Velocity[Y]             -3.5343          5.1603         0.24963         0.19114
v  Velocity[Z]             -6.0446          3.5772        -0.20222     -0.00068522
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13319E+01 0.14050E+01
   Friction velocity        uet   :  0.20280E-01 0.17432E+02
   Friction velocity        uk    :  0.20060E-01 0.17432E+02
   Dimensionless distance   yplus :  0.22244E-02 0.92086E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2520
   Nb of faces within the viscous sub-layer     :      28955
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42702E+00     374   0.15787E+00   0.12096E+00 0.20975E+01 
c  Velocity[X]                                      0.29319E-01 
c  Velocity[Y]                                      0.46700E-01 
c  Velocity[Z]                                      0.44937E-01 
c  Pressure     0.22470E-01     919   0.21125E-01   0.52995E-01 0.65420E-01 
c  k            0.15177E-01     163   0.25103E-03   0.22107E-04 0.30184E+01 
c  epsilon      0.86815E+02     132   0.37125E-03   0.61932E+03 0.96462E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.4592e-05                             6
a  epsilon              -0.0071955                             9
a  Local Time Step      4.2278e-08                        281552


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8844          3.5181         0.35385        0.080856
v  Velocity[Y]             -3.5343          5.1603         0.24963         0.19114
v  Velocity[Z]             -6.0446          3.5772        -0.20222     -0.00068522
v  ǁVelocityǁ           0.00070052           6.715          1.2236          1.5789
v  Pressure                -938.38           14868          9824.3          8056.8
v  k                    5.5485e-09         0.35864       0.0042512        0.008016
v  epsilon              0.00013022            5442          10.518          3.8708
v  TurbVisc             4.2298e-14          0.1418      0.00048838       0.0064211
v  CourantNb              0.022432           46256          71.208          17.215
v  FourierNb               0.22218      2.3653e+06          217.37          2.7604
v  total_pressure       4.9906e+05      5.1487e+05      5.0982e+05      5.0806e+05
v  Local Time Step            0.01        0.066992        0.010004        0.010015


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5604      2.3904e+06          288.58          19.976


 TIME FOR THE TIME STEP              133:        0.20585E+03

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


 INSTANT    0.134000000E+02   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        -0.500827957E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640981E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13366E+01 0.14093E+01
   Friction velocity        uet   :  0.18689E-01 0.16684E+02
   Friction velocity        uk    :  0.18486E-01 0.16684E+02
   Dimensionless distance   yplus :  0.21289E-02 0.92155E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2508
   Nb of faces within the viscous sub-layer     :      28954
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-------------
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5811      2.3887e+06          288.52          19.976


 TIME FOR THE TIME STEP              134:        0.20280E+03

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


 INSTANT    0.135000000E+02   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        -0.520319207E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640666E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13430E+01 0.14166E+01
   Friction velocity        uet   :  0.18541E-01 0.16575E+02
   Friction velocity        uk    :  0.18307E-01 0.16575E+02
   Dimensionless distance   yplus :  0.20972E-02 0.92263E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2509
   Nb of faces within the viscous sub-layer     :      28954
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
------------------------------------------------------------------
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5811      2.3887e+06          288.52          19.976


 TIME FOR THE TIME STEP              134:        0.20669E+03

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


 INSTANT    0.135000000E+02   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        -0.520319207E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640666E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13430E+01 0.14166E+01
   Friction velocity        uet   :  0.18541E-01 0.16575E+02
   Friction velocity        uk    :  0.18307E-01 0.16575E+02
   Dimensionless distance   yplus :  0.20972E-02 0.92263E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2509
   Nb of faces within the viscous sub-layer     :      28954
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42719E+00     359   0.16118E+00   0.11931E+00 0.20832E+01 
c  Velocity[X]                                      0.28439E-01 
c  Velocity[Y]                                      0.43989E-01 
c  Velocity[Z]                                      0.46881E-01 
c  Pressure     0.22173E-01     855   0.20559E-01   0.52258E-01 0.46472E-01 
c  k            0.15171E-01     151   0.29588E-03   0.16621E-04 0.26153E+01 
c  epsilon      0.86807E+02     120   0.44531E-03   0.85266E+03 0.11332E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.6757e-05                             5
a  epsilon               -0.010673                             4
a  Local Time Step      4.2278e-08                        281553


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.1147          3.5308         0.35459        0.080878
v  Velocity[Y]             -3.5162          5.2202         0.25014         0.19141
v  Velocity[Z]             -6.0206          3.5652        -0.20204     -0.00059147
v  ǁVelocityǁ           0.00025386          6.7001          1.2241          1.5786
v  Pressure                -938.29           14867          9823.4          8056.4
v  k                    5.4416e-09         0.35503       0.0042625       0.0080258
v  epsilon              0.00013014          5366.8          10.536          3.8705
v  TurbVisc              5.009e-14          0.1418      0.00048991       0.0064252
v  CourantNb             0.0099896           48394          71.172           17.21
v  FourierNb               0.22221      2.3653e+06          217.37          2.7605
v  total_pressure       4.9906e+05      5.1487e+05      5.0982e+05      5.0806e+05
v  Local Time Step            0.01         0.06602        0.010004        0.010014


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6125      2.3886e+06          288.54          19.971


 TIME FOR THE TIME STEP              135:        0.18958E+03

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


 INSTANT    0.136000000E+02   TIME STEP NUMBER             136
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.69964a  k                   -2.5625e-05                             5
a  epsilon               -0.012091                             3
a  Local Time Step      4.2278e-08                        281563


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.0658          3.5253         0.35513        0.080835
v  Velocity[Y]             -3.4869          5.2768         0.25074         0.19157
v  Velocity[Z]             -5.9246          3.5864        -0.20208     -0.00048137
v  ǁVelocityǁ            0.0003522          6.5919          1.2246          1.5784
v  Pressure                -938.25           14866          9821.8          8056.1
v  k                    6.5056e-09         0.35548       0.0042619       0.0080322
v  epsilon              0.00013039          5377.8          10.482          3.8755
v  TurbVisc             3.8557e-14          0.1418      0.00049044       0.0064269
v  CourantNb              0.034978           48005          71.149          17.211
v  FourierNb               0.22221      2.3653e+06          217.37          2.7611
v  total_pressure       4.9906e+05      5.1487e+05      5.0982e+05      5.0806e+05
v  Local Time Step            0.01        0.071926        0.010004        0.010014


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6416      2.3879e+06          288.52          19.972


 TIME FOR THE TIME STEP              136:        0.19819E+03

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


 INSTANT    0.137000000E+02   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        -0.931425118E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outa  k                   -2.5625e-05                             5
a  epsilon               -0.012091                             3
a  Local Time Step      4.2278e-08                        281563


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.0658          3.5253         0.35513        0.080835
v  Velocity[Y]             -3.4869          5.2768         0.25074         0.19157
v  Velocity[Z]             -5.9246          3.5864        -0.20208     -0.00048137
v  ǁVelocityǁ            0.0003522          6.5919          1.2246          1.5784
v  Pressure                -938.25           14866          9821.8          8056.1
v  k                    6.5056e-09         0.35548       0.0042619       0.0080322
v  epsilon              0.00013039          5377.8          10.482          3.8755
v  TurbVisc             3.8557e-14          0.1418      0.00049044       0.0064269
v  CourantNb              0.034978           48005          71.149          17.211
v  FourierNb               0.22221      2.3653e+06          217.37          2.7611
v  total_pressure       4.9906e+05      5.1487e+05      5.0982e+05      5.0806e+05
v  Local Time Step            0.01        0.071926        0.010004        0.010014


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6416      2.3879e+06          288.52          19.972


 TIME FOR THE TIME STEP              136:        0.20291E+03

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


 INSTANT    0.137000000E+02   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        -0.931425118E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699641010E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13280E+01 0.14056E+01
   Friction velocity        uet   :  0.11588E-01 0.16814E+02
   Friction velocity        uk    :  0.11585E-01 0.16814E+02
   Dimensionless distance   yplus :  0.16614E-02 0.92032E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2504
   Nb of faces within the viscous sub-layer     :      28953
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42727E+00     351   0.16135E+00   0.11309E+00 0.20285E+01 
c  Velocity[X]                                      0.28104E-01 
c  Velocity[Y]                                      0.42071E-01 
c  Velocity[Z]                                      0.42912E-01 
c  Pressure     0.20839E-01     977   0.19293E-01   0.49002E-01 0.75814E-01 
c  k            0.15183E-01     156   0.28364E-03   0.16078E-04 0.25692E+01 
c  epsilon      0.86232E+02     121   0.50694E-03   0.71808E+03 0.10335E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.2271e-05                             5
a  epsilon               -0.010501                             4
a  Local Time Step      4.2278e-08                        281566


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9718          3.5425         0.35534        0.080762
v  Velocity[Y]             -3.5064          5.2272         0.25051         0.19174
v  Velocity[Z]             -5.8811          3.5871        -0.20173     -0.00037006
v  ǁVelocityǁ           0.00043042          6.5738          1.2247          1.5784
v  Pressure                -940.08           14857            9814         Dimensionless distance   yplus :  0.15717E-02 0.91672E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2506
   Nb of faces within the viscous sub-layer     :      28947
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42738E+00     351   0.16395E+00   0.11389E+00 0.20359E+01 
c  Velocity[X]                                      0.28675E-01 
c  Velocity[Y]                                      0.42356E-01 
c  Velocity[Z]                                      0.42862E-01 
c  Pressure     0.20186E-01     960   0.18341E-01   0.47408E-01 0.56080E-01 
c  k            0.15182E-01     143   0.26329E-03   0.15446E-04 0.25184E+01 
c  epsilon      0.85890E+02     150   0.38599E-03   0.64157E+03 0.97835E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.1567e-05                            11
a  epsilon               -0.093678                            19
a  Local Time Step      4.2278e-08                        281572


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.0148          3.5584         0.35631        0.080758
v  Velocity[Y]             -3.4926          5.2571         0.25046         0.19191
v  Velocity[Z]             -5.9575          3.5849        -0.20131      -0.0003191
v  ǁVelocityǁ           0.00058587          6.6144          1.2249          1.5783
v  Pressure                -945.98           14851          9809.1          8048.5
v  k                    5.4727e-09         0.36026       0.0042705       0.0080382
v  epsilon              0.00013059            5495          10.556          3.8861
v  TurbVisc             4.5541e-   Dimensionless distance   yplus :  0.15717E-02 0.91672E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2506
   Nb of faces within the viscous sub-layer     :      28947
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42738E+00     351   0.16395E+00   0.11389E+00 0.20359E+01 
c  Velocity[X]                                      0.28675E-01 
c  Velocity[Y]                                      0.42356E-01 
c  Velocity[Z]                                      0.42862E-01 
c  Pressure     0.20186E-01     960   0.18341E-01   0.47408E-01 0.56080E-01 
c  k            0.15182E-01     143   0.26329E-03   0.15446E-04 0.25184E+01 
c  epsilon      0.85890E+02     150   0.38599E-03   0.64157E+03 0.97835E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.1567e-05                            11
a  epsilon               -0.093678                            19
a  Local Time Step      4.2278e-08                        281572


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.0148          3.5584         0.35631        0.080758
v  Velocity[Y]             -3.4926          5.2571         0.25046         0.19191
v  Velocity[Z]             -5.9575          3.5849        -0.20131      -0.0003191
v  ǁVelocityǁ           0.00058587          6.6144          1.2249          1.5783
v  Pressure                -945.98           14851          9809.1          8048.5
v  k                    5.4727e-09         0.36026       0.0042705       0.0080382
v  epsilon              0.00013059            5495          10.556          3.8861
v  TurbVisc             4.5541e-14          0.1418      0.00049121       0.0064295
v  CourantNb              0.012032           49736           71.17          17.208
v  FourierNb               0.22221      2.3653e+06          217.38          2.7607
v  total_pressure       4.9905e+05      5.1485e+05      5.0981e+05      5.0805e+05
v  Local Time Step            0.01         0.08242        0.010004        0.010013


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6512      2.3881e+06          288.55          19.969


 TIME FOR THE TIME STEP              138:        0.17305E+03

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


 INSTANT    0.139000000E+02   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        -0.120190442E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699641010E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12968E+01 0.13903E+01
   Friction velocity        uet   :  0.13257E-01 0.14072E+02
   Friction velocity        uk    :  0.13214E-01 0.14072E+02
   Dimensionless distance   yplus :  0.16754E-02 0.91550E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2501
   Nb of faces within the viscous sub-layer     :      28930
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42679E+00     347   0.16040E+00   0.11704E+00 0.20640E+01 
c  Velocity[X]                                      0.28453E-01 
c  Velocity[Y]    INSTANT    0.140000000E+02   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        -0.607517171E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12670E+01 0.13940E+01
   Friction velocity        uet   :  0.73615E-02 0.14448E+02
   Friction velocity        uk    :  0.73353E-02 0.14448E+02
   Dimensionless distance   yplus :  0.66847E-03 0.91059E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2508
   Nb of faces within the viscous sub-layer     :      28938
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42686E+00     342   0.15766E+00   0.11851E+00 0.20772E+01 
c  Velocity[X]                                      0.29906E-01 
c  Velocity[Y]                                      0.45426E-01 
c  Velocity[Z]                                      0.43182E-01 
c  Pressure     0.20715E-01     975   0.18327E-01   0.48529E-01 0.71739E-01 
c  k            0.1 INSTANT    0.140000000E+02   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        -0.607517171E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640992E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12670E+01 0.13940E+01
   Friction velocity        uet   :  0.73615E-02 0.14448E+02
   Friction velocity        uk    :  0.73353E-02 0.14448E+02
   Dimensionless distance   yplus :  0.66847E-03 0.91059E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2508
   Nb of faces within the viscous sub-layer     :      28938
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42686E+00     342   0.15766E+00   0.11851E+00 0.20772E+01 
c  Velocity[X]                                      0.29906E-01 
c  Velocity[Y]                                      0.45426E-01 
c  Velocity[Z]                                      0.43182E-01 
c  Pressure     0.20715E-01     975   0.18327E-01   0.48529E-01 0.71739E-01 
c  k            0.15186E-01     145   0.22542E-03   0.13830E-04 0.23830E+01 
c  epsilon      0.85766E+02     174   0.22979E-03   0.33353E+03 0.70526E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.2887e-05                             9
a  epsilon               -0.084148                            13
a  Local Time Step      4.2278e-08                        281583


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9661          3.5519         0.35714        0.080776
v  Velocity[Y]             -3.4853          5.2008         0.25085         0.19208
v  Velocity[Z]             -5.8894          3.6039         -0.2001     -0.00029196
v  ǁVelocityǁ           0.00055867          6.5361          1.2248           1.578
v  Pressure                -968.71           14834            9792          8038.2
v  k                    5.5489e-09         0.35513       0.0042782       0.0080395
v  epsilon               0.0001194          5370.9          10.584          3.8893
v  TurbVisc             4.9109e-14          0.1418      0.00049026       0.0064299
v  CourantNb              0.012114           51431          71.151          17.207
v  FourierNb                0.2222      2.3653e+06          217.38          2.7602
v  total_pressure       4.9903e+05      5.1483e+05      5.0979e+05      5.0804e+05
v  Local Time Step            0.01        0.063906        0.010004        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6962      2.3874e+06          288.53          19.967


 TIME FOR THE TIME STEP              140:        0.17602E+03

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


 INSTANT    0.141000000E+02   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        -0.558006482E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640996E+00
Free inlet               13           0         0.000000000E+00
Convective i-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9944          3.5272         0.35725        0.080658
v  Velocity[Y]             -3.5054          5.1876         0.25068         0.19195
v  Velocity[Z]             -5.8846          3.5938         -0.1997      -0.0003758
v  ǁVelocityǁ           0.00057411          6.5621          1.2247           1.578
v  Pressure                -980.08           14821          9779.3          8029.9
v  k                    5.5018e-09         0.35817       0.0042769       0.0080372
v  epsilon              9.3218e-05            5444          10.603          3.8885
v  TurbVisc             4.0652e-14          0.1418      0.00048941       0.0064292
v  CourantNb            0.00087243           49881          71.084          17.205
v  FourierNb               0.22218      2.3653e+06          217.38          2.7606
v  total_pressure       4.9902e+05      5.1482e+05      5.0978e+05      5.0803e+05
v  Local Time Step            0.01        0.070297        0.010004        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.689      2.3852e+06          288.46          19.966


 TIME FOR THE TIME STEP              141:        0.18640E+03

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


 INSTANT    0.142000000E+02   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        -0.407925691E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
------------------------------  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9944          3.5272         0.35725        0.080658
v  Velocity[Y]             -3.5054          5.1876         0.25068         0.19195
v  Velocity[Z]             -5.8846          3.5938         -0.1997      -0.0003758
v  ǁVelocityǁ           0.00057411          6.5621          1.2247           1.578
v  Pressure                -980.08           14821          9779.3          8029.9
v  k                    5.5018e-09         0.35817       0.0042769       0.0080372
v  epsilon              9.3218e-05            5444          10.603          3.8885
v  TurbVisc             4.0652e-14          0.1418      0.00048941       0.0064292
v  CourantNb            0.00087243           49881          71.084          17.205
v  FourierNb               0.22218      2.3653e+06          217.38          2.7606
v  total_pressure       4.9902e+05      5.1482e+05      5.0978e+05      5.0803e+05
v  Local Time Step            0.01        0.070297        0.010004        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.689      2.3852e+06          288.46          19.966


 TIME FOR THE TIME STEP              141:        0.19337E+03

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


 INSTANT    0.142000000E+02   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        -0.407925691E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12144E+01 0.13969E+01
   Friction velocity        uet   :  0.13538E-01 0.14194E+02
   Friction velocity        uk    :  0.13535E-01 0.14194E+02
   Dimensionless distance   yplus :  0.16168E-02 0.90203E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2510
   Nb of faces within the viscous sub-layer     :      28931
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42667E+00     337   0.15811E+00   0.11726E+00 0.20665E+01 
c  Velocity[X]                                      0.30989E-01 
c  Velocity[Y]                                      0.42706E-01 
c  Velocity[Z]                                      0.43565E-01 
c  Pressure     0.22278E-01    1083   0.19468E-01   0.52169E-01 0.15167E+00 
c  k            0.15190E-01     142   0.19361E-03   0.10081E-04 0.20346E+01 
c  epsilon      0.86155E+02     142   0.24456E-03   0.22242E+03 0.57481E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.8394e-05                             3
a  epsilon                 -4.2384                             8
a  Local Time Step      4.2278e-08                        281591


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.0152           3.537         0.35741        0.080556
v  Velocity[Y]             -3.4946          5.1245          0.2505         0.19189
v  Velocity[Z]             -5.8775          3.6187        -0.19937     -0.00047546
v  ǁVelocityǁ           0.00088759          6.5388          1.2242          1.5778
v  Pressure                -991.94           14802          9761.4          8017.9
v  k                    6.9975e-09         0.35888       0.0042837       0.0080368
v  epsilon              6.8699e-05          5465.1            10.6          3.8926
v  TurbVisc             3.9508e-14          0.1418      0.00048925       0.0064288
v  CourantNb              0.023779        ------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42639E+00     345   0.15685E+00   0.12010E+00 0.20915E+01 
c  Velocity[X]                                      0.30623E-01 
c  Velocity[Y]                                      0.42489E-01 
c  Velocity[Z]                                      0.46986E-01 
c  Pressure     0.22349E-01    1082   0.19389E-01   0.52293E-01 0.17606E+00 
c  k            0.15183E-01     144   0.21142E-03   0.97540E-05 0.20015E+01 
c  epsilon      0.85449E+02     120   0.27465E-03   0.20057E+03 0.54641E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.3486e-05                            14
a  epsilon                -0.23512                            22
a  Local Time Step      4.2278e-08                        281593


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9382          3.5498         0.35715        0.080524
v  Velocity[Y]             -3.5065           5.125         0.25011         0.19179
v  Velocity[Z]             -5.9753          3.6136        -0.19847     -0.00052293
v  ǁVelocityǁ           0.00066406          6.6412          1.2231          1.5778
v  Pressure                -1001.3           14780          9740.8          8003.5
v  k                    5.5628e-09         0.35951       0.0042817       0.0080337
v  epsilon              5.0661e-05          5476.4          10.622          3.8887
v  TurbVisc             5.0865e-14          0.1418      0.00048914       0.0064282
v  CourantNb              0.011167           50421          71.039          17.199
v  FourierNb               0.22215      2.3653e+06          217.38          2.7606
v  total_pressure         4.99e+05      5.1478e+05      5.0974e+05        5.08e+05
v ------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42639E+00     345   0.15685E+00   0.12010E+00 0.20915E+01 
c  Velocity[X]                                      0.30623E-01 
c  Velocity[Y]                                      0.42489E-01 
c  Velocity[Z]                                      0.46986E-01 
c  Pressure     0.22349E-01    1082   0.19389E-01   0.52293E-01 0.17606E+00 
c  k            0.15183E-01     144   0.21142E-03   0.97540E-05 0.20015E+01 
c  epsilon      0.85449E+02     120   0.27465E-03   0.20057E+03 0.54641E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.3486e-05                            14
a  epsilon                -0.23512                            22
a  Local Time Step      4.2278e-08                        281593


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9382          3.5498         0.35715        0.080524
v  Velocity[Y]             -3.5065           5.125         0.25011         0.19179
v  Velocity[Z]             -5.9753          3.6136        -0.19847     -0.00052293
v  ǁVelocityǁ           0.00066406          6.6412          1.2231          1.5778
v  Pressure                -1001.3           14780          9740.8          8003.5
v  k                    5.5628e-09         0.35951       0.0042817       0.0080337
v  epsilon              5.0661e-05          5476.4          10.622          3.8887
v  TurbVisc             5.0865e-14          0.1418      0.00048914       0.0064282
v  CourantNb              0.011167           50421          71.039          17.199
v  FourierNb               0.22215      2.3653e+06          217.38          2.7606
v  total_pressure         4.99e+05      5.1478e+05      5.0974e+05        5.08e+05
v  Local Time Step            0.01        0.069569        0.010004        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.709      2.3865e+06          288.42           19.96


 TIME FOR THE TIME STEP              143:        0.18593E+03

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


 INSTANT    0.144000000E+02   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        -0.552882219E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11581E+01 0.13899E+01
   Friction velocity        uet   :  0.96799E-02 0.14188E+02
   Friction velocity        uk    :  0.96373E-02 0.14188E+02
   Dimensionless distance   yplus :  0.18103E-02 0.88069E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2500
   Nb of faces within the viscous sub-layer     :      28926
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42635E+00     335   0.15865E+00   0.12158E+00 0.21046E+01 
c  Velocity[X]                                      0.31265E-01 
c  Velocity[Y]                                      0.46273E-01 
c  Velocity[Z]                                      0.44046E-01 
c  Pressure     0.22657E-01    1101   0.19726E-01   0.53006E-01 0.17748E+00 
c  k            0.15176E-01     134   0.19830E-03   0.91159E-05 0.19352E+01 
c  Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.360993779E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699641010E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11603E+01 0.13825E+01
   Friction velocity        uet   :  0.12291E-01 0.14490E+02
   Friction velocity        uk    :  0.12228E-01 0.14490E+02
   Dimensionless distance   yplus :  0.18489E-02 0.88688E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2497
   Nb of faces within the viscous sub-layer     :      28936
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42609E+00     337   0.15991E+00   0.12551E+00 0.21380E+01 
c  Velocity[X]                                      0.34928E-01 
c  Velocity[Y]                                      0.45663E-01 
c  Velocity[Z]                                      0.44915E-01 
c  Pressure     0.22922E-01    1100   0.19929E-01   0.53586E-01 0.16308E+00 
c  k            0.15171E-01     125   0.21875E-03   0.13150E-04 0.23241E+01 
c  epsilon      0.84510E+02     113   0.39690E-03   0.47212E+03 0.83838E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     ----------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.360993779E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699641010E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11603E+01 0.13825E+01
   Friction velocity        uet   :  0.12291E-01 0.14490E+02
   Friction velocity        uk    :  0.12228E-01 0.14490E+02
   Dimensionless distance   yplus :  0.18489E-02 0.88688E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2497
   Nb of faces within the viscous sub-layer     :      28936
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42609E+00     337   0.15991E+00   0.12551E+00 0.21380E+01 
c  Velocity[X]                                      0.34928E-01 
c  Velocity[Y]                                      0.45663E-01 
c  Velocity[Z]                                      0.44915E-01 
c  Pressure     0.22922E-01    1100   0.19929E-01   0.53586E-01 0.16308E+00 
c  k            0.15171E-01     125   0.21875E-03   0.13150E-04 0.23241E+01 
c  epsilon      0.84510E+02     113   0.39690E-03   0.47212E+03 0.83838E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.0572e-05                             8
a  epsilon                -0.18103                            21
a  Local Time Step      4.2278e-08                        281593


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8637          3.5421          0.3574        0.080447
v  Velocity[Y]             -3.5024          5.1389         0.24952         0.19201
v  Velocity[Z]             -6.0045          3.6142        -0.19787     -0.00051911
v  ǁVelocityǁ           0.00043644          6.6587          1.2226          1.5774
v  Pressure                -998.95           14736          9700.9          7976.1
v  k                    6.4844e-09         0.36126       0.0042804       0.0080278
v  epsilon               4.142e-05          5495.9          10.633          3.8841
v  TurbVisc             4.6712e-14          0.1418       0.0004885       0.0064273
v  CourantNb              0.003282           51189          70.958          17.191
v  FourierNb               0.22211      2.3653e+06          217.38          2.7603
v  total_pressure         4.99e+05      5.1474e+05       5.097e+05      5.0798e+05
v  Local Time Step            0.01        0.084179        0.010004        0.010011


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7169      2.3868e+06          288.33          19.951


 TIME FOR THE TIME STEP              145:        0.16397E+03

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


 INSTANT    0.146000000E+02   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        -0.660421133E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699641012E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   v  Velocity[Z]              -5.963          3.6223        -0.19788     -0.00053727
v  ǁVelocityǁ           0.00078679          6.6148          1.2223          1.5769
v  Pressure                -990.82           14719          9685.3          7965.4
v  k                    6.5786e-09         0.35274       0.0042759       0.0080267
v  epsilon              4.4506e-05          5310.1          10.579           3.883
v  TurbVisc             4.7151e-14          0.1418      0.00048887       0.0064273
v  CourantNb               0.05168           51943          70.904          17.192
v  FourierNb               0.22208      2.3653e+06          217.38           2.761
v  total_pressure       4.9901e+05      5.1472e+05      5.0969e+05      5.0797e+05
v  Local Time Step            0.01        0.092596        0.010004        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7192      2.3832e+06          288.28          19.953


 TIME FOR THE TIME STEP              146:        0.15644E+03

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


 INSTANT    0.147000000E+02   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        -0.548161378E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
----v  Velocity[Z]              -5.963          3.6223        -0.19788     -0.00053727
v  ǁVelocityǁ           0.00078679          6.6148          1.2223          1.5769
v  Pressure                -990.82           14719          9685.3          7965.4
v  k                    6.5786e-09         0.35274       0.0042759       0.0080267
v  epsilon              4.4506e-05          5310.1          10.579           3.883
v  TurbVisc             4.7151e-14          0.1418      0.00048887       0.0064273
v  CourantNb               0.05168           51943          70.904          17.192
v  FourierNb               0.22208      2.3653e+06          217.38           2.761
v  total_pressure       4.9901e+05      5.1472e+05      5.0969e+05      5.0797e+05
v  Local Time Step            0.01        0.092596        0.010004        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7192      2.3832e+06          288.28          19.953


 TIME FOR THE TIME STEP              146:        0.15673E+03

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


 INSTANT    0.147000000E+02   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        -0.548161378E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11771E+01 0.13840E+01
   Friction velocity        uet   :  0.13128E-01 0.13453E+02
   Friction velocity        uk    :  0.13125E-01 0.13453E+02
   Dimensionless distance   yplus :  0.17167E-02 0.86282E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2489
   Nb of faces within the viscous sub-layer     :      28931
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42587E+00     338   0.15387E+00   0.13095E+00 0.21847E+01 
c  Velocity[X]                                      0.35460E-01 
c  Velocity[Y]                                      0.46066E-01 
c  Velocity[Z]                                      0.49422E-01 
c  Pressure     0.23159E-01    1063   0.20083E-01   0.54100E-01 0.12442E+00 
c  k            0.15158E-01     152   0.22200E-03   0.12849E-04 0.22986E+01 
c  epsilon      0.84376E+02     144   0.21704E-03   0.25204E+03 0.61366E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.3682e-05                            13
a  epsilon                -0.20757                            24
a  Local Time Step      4.2278e-08                        281594


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8453          3.5333         0.35699        0.080548
v  Velocity[Y]             -3.5048          5.1938         0.24908         0.19229
v  Velocity[Z]             -6.0443          3.6096        -0.19756      -0.0005309
v  ǁVelocityǁ           0.00059556          6.6964          1.2217          1.5768
v  Pressure                -979.96           14703          9671.4          7955.7
v  k                    6.5558e-09         0.35667       0.0042733        0.008021
v  epsilon              4.9084e-05          5386.5          10.613          3.8765
v  TurbVisc             4.7576e-14          0.1418      0.00048824       0.0064268
v  CourantNb              0.018187           51994          70.886          17.187
v  FourierNb               0.22204      2.3653e+06          217.38          2.7605
v  total_pressure       4.9902e+05       5.147e+05      5.0967e+05      5.0796e+05
v  Local Time Step            0.01        0.097219        0.010004        0.010-----------------------------------------------------------------------------
c  Velocity     0.42592E+00     329   0.15624E+00   0.12203E+00 0.21091E+01 
c  Velocity[X]                                      0.32939E-01 
c  Velocity[Y]                                      0.41453E-01 
c  Velocity[Z]                                      0.47633E-01 
c  Pressure     0.23209E-01    1011   0.20060E-01   0.54169E-01 0.94614E-01 
c  k            0.15159E-01     137   0.20047E-03   0.11385E-04 0.21640E+01 
c  epsilon      0.85203E+02     162   0.33864E-03   0.30748E+03 0.67782E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.9958e-05                            16
a  epsilon               -0.092609                            24
a  Local Time Step      4.2278e-08                        281599


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9911            3.56         0.35684        0.080718
v  Velocity[Y]             -3.4864          5.2017         0.24886         0.19237
v  Velocity[Z]             -5.9986           3.618        -0.19742     -0.00058932
v  ǁVelocityǁ           0.00061907          6.6425          1.2212          1.5766
v  Pressure                -965.14           14692          9661.2          7948.6
v  k                     1.253e-09         0.35424       0.0042681       0.0080178
v  epsilon              1.8071e-05          5335.5          10.594          3.8764
v  TurbVisc             4.7191e-14          0.1418      0.00048755       0.0064264
v  CourantNb              0.010776           52361          70.851          17.187
v  FourierNb               0.22201      2.3653e+06          217.38          2.7607
v  total_pressure       4.9903e+05      5.1469e+05      5.0966e+05      5.0795e+05
v  Local Time Step            0.01         0.10694        0.010004        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  ------------------------------------------------------------------------------------
c  Velocity     0.42592E+00     329   0.15624E+00   0.12203E+00 0.21091E+01 
c  Velocity[X]                                      0.32939E-01 
c  Velocity[Y]                                      0.41453E-01 
c  Velocity[Z]                                      0.47633E-01 
c  Pressure     0.23209E-01    1011   0.20060E-01   0.54169E-01 0.94614E-01 
c  k            0.15159E-01     137   0.20047E-03   0.11385E-04 0.21640E+01 
c  epsilon      0.85203E+02     162   0.33864E-03   0.30748E+03 0.67782E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.9958e-05                            16
a  epsilon               -0.092609                            24
a  Local Time Step      4.2278e-08                        281599


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9911            3.56         0.35684        0.080718
v  Velocity[Y]             -3.4864          5.2017         0.24886         0.19237
v  Velocity[Z]             -5.9986           3.618        -0.19742     -0.00058932
v  ǁVelocityǁ           0.00061907          6.6425          1.2212          1.5766
v  Pressure                -965.14           14692          9661.2          7948.6
v  k                     1.253e-09         0.35424       0.0042681       0.0080178
v  epsilon              1.8071e-05          5335.5          10.594          3.8764
v  TurbVisc             4.7191e-14          0.1418      0.00048755       0.0064264
v  CourantNb              0.010776           52361          70.851          17.187
v  FourierNb               0.22201      2.3653e+06          217.38          2.7607
v  total_pressure       4.9903e+05      5.1469e+05      5.0966e+05      5.0795e+05
v  Local Time Step            0.01         0.10694        0.010004        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7198       2.384e+06          288.23          19.947


 TIME FOR THE TIME STEP              148:        0.14634E+03

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


 INSTANT    0.149000000E+02   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        -0.328645069E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640994E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12020E+01 0.13841E+01
   Friction velocity        uet   :  0.69736E-02 0.13046E+02
   Friction velocity        uk    :  0.69717E-02 0.13046E+02
   Dimensionless distance   yplus :  0.16646E-02 0.84921E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2484
   Nb of faces within the viscous sub-layer     :      28933
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42586E+00     330   0.15488E+00   0.11715E+00 0.20668E+01 
c  Velocity[X]                                      0.31629E-01 
c  Velocity[Y]                                      0.39899E-01 
c  Velocity[Z]                                      0.45625E-01 
c  Pressure     0.21792E-01    1047   0.18682E-01   0.50837E-01 0.10317E+00 
c  k            0.15144E-01     143   0.19145E-03   0.10957E-04 0.21239E+01 
c  epsilon      0.84171E+02     142   0.27185E-03   0.26805E+03 0.63537E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ----Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12174E+01 0.13907E+01
   Friction velocity        uet   :  0.94526E-02 0.13236E+02
   Friction velocity        uk    :  0.94500E-02 0.13236E+02
   Dimensionless distance   yplus :  0.16890E-02 0.85129E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2479
   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     0.42585E+00     322   0.15229E+00   0.10851E+00 0.19893E+01 
c  Velocity[X]                                      0.30002E-01 
c  Velocity[Y]                                      0.36993E-01 
c  Velocity[Z]                                      0.41516E-01 
c  Pressure     0.20471E-01     975   0.17584E-01   0.47738E-01 0.62858E-01 
c  k            0.15149E-01     150   0.17855E-03   0.98776E-05 0.20167E+01 
c  epsilon      0.85479E+02     234   0.23968E-03   0.23364E+03 0.59050E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.7377e-05                             7
a  epsilon                -0.18922                            15
a  LocaSymmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12174E+01 0.13907E+01
   Friction velocity        uet   :  0.94526E-02 0.13236E+02
   Friction velocity        uk    :  0.94500E-02 0.13236E+02
   Dimensionless distance   yplus :  0.16890E-02 0.85129E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2479
   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     0.42585E+00     322   0.15229E+00   0.10851E+00 0.19893E+01 
c  Velocity[X]                                      0.30002E-01 
c  Velocity[Y]                                      0.36993E-01 
c  Velocity[Z]                                      0.41516E-01 
c  Pressure     0.20471E-01     975   0.17584E-01   0.47738E-01 0.62858E-01 
c  k            0.15149E-01     150   0.17855E-03   0.98776E-05 0.20167E+01 
c  epsilon      0.85479E+02     234   0.23968E-03   0.23364E+03 0.59050E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.7377e-05                             7
a  epsilon                -0.18922                            15
a  Local Time Step      4.2278e-08                        281602


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9634          3.5492         0.35676        0.081045
v  Velocity[Y]              -3.487          5.2714         0.24928          0.1923
v  Velocity[Z]             -6.0423           3.595        -0.19757     -0.00052533
v  ǁVelocityǁ           0.00050998          6.6869          1.2211           1.576
v  Pressure                -959.89           14672          9643.7          7935.7
v  k                    5.8865e-09          0.3527       0.0042643       0.0080068
v  epsilon              5.6373e-05          5314.5          10.581          3.8698
v  TurbVisc             4.7608e-14          0.1418      0.00048653       0.0064249
v  CourantNb              0.020188           51136          70.799          17.182
v  FourierNb               0.22195      2.3653e+06          217.37          2.7606
v  total_pressure       4.9904e+05      5.1467e+05      5.0964e+05      5.0794e+05
v  Local Time Step            0.01        0.083916        0.010003        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7203      2.3854e+06          288.17          19.943


 TIME FOR THE TIME STEP              150:        0.14848E+03

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


 INSTANT    0.151000000E+02   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        -0.478083321E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12255E+01 0.13851E+01
   Fricv  epsilon              2.8525e-05          5495.7          10.601           3.864
v  TurbVisc             4.2517e-14          0.1418      0.00048561       0.0064236
v  CourantNb             0.0099743           51744          70.852          17.178
v  FourierNb               0.22192      2.3653e+06          217.37          2.7599
v  total_pressure       4.9905e+05      5.1467e+05      5.0964e+05      5.0793e+05
v  Local Time Step            0.01        0.092308        0.010004        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7045      2.3879e+06          288.23          19.938


 TIME FOR THE TIME STEP              151:        0.14042E+03

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


 INSTANT    0.152000000E+02   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        -0.701806805E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12407E+01 0.13903E+01
   Friction velocity        uet   :  0.69171E-02 0.13060E+02
   Friction velocity        uk    :  0.69152E-02 0.13060E+02
   Dimensionless distance   yplus :  0.15458E-02 0.85306E+01
   ------------------------------v  epsilon              2.8525e-05          5495.7          10.601           3.864
v  TurbVisc             4.2517e-14          0.1418      0.00048561       0.0064236
v  CourantNb             0.0099743           51744          70.852          17.178
v  FourierNb               0.22192      2.3653e+06          217.37          2.7599
v  total_pressure       4.9905e+05      5.1467e+05      5.0964e+05      5.0793e+05
v  Local Time Step            0.01        0.092308        0.010004        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7045      2.3879e+06          288.23          19.938


 TIME FOR THE TIME STEP              151:        0.14110E+03

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


 INSTANT    0.152000000E+02   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        -0.701806805E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12407E+01 0.13903E+01
   Friction velocity        uet   :  0.69171E-02 0.13060E+02
   Friction velocity        uk    :  0.69152E-02 0.13060E+02
   Dimensionless distance   yplus :  0.15458E-02 0.85306E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2471
   Nb of faces within the viscous sub-layer     :      28936
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42651E+00     335   0.15550E+00   0.10071E+00 0.19165E+01 
c  Velocity[X]                                      0.26747E-01 
c  Velocity[Y]                                      0.35712E-01 
c  Velocity[Z]                                      0.38250E-01 
c  Pressure     0.17851E-01     902   0.14662E-01   0.41622E-01 0.42991E-01 
c  k            0.15153E-01     144   0.17231E-03   0.86064E-05 0.18832E+01 
c  epsilon      0.85689E+02     156   0.19921E-03   0.23518E+03 0.59094E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012272                             9
a  epsilon                 -0.3683                            18
a  Local Time Step      4.2278e-08                        281604


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8275          3.5602         0.35717        0.081307
v  Velocity[Y]             -3.4807          5.2737          0.2497          0.1924
v  Velocity[Z]             -6.0693          3.6007        -0.19746     -0.00054034
v  ǁVelocityǁ           0.00060797          6.7098          1.2219          1.5757
v  Pressure                -945.17           14665          9635.5          7929.8
v  k                    5.7537e-09         0.35365       0.0042649       0.0079972
v  epsilon              5.8773e-05          5337.7           10.61          3.8673
v  TurbVisc             5.0895e-14          0.1418      0.00048517       0.0064224
v  CourantNb              0.015346           51281          70.893          17.181
v  FourierNb               0.22189      2.3653e+06          217.37          2.7598
v  total_pressure       4.9905e+05      5.1466e+05      5.0964e+05      5.0793e+05
v  Local Time Step            0.01         0.10154        0.010003        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7076      2.3888e+06  c  Velocity[Z]                                      0.39193E-01 
c  Pressure     0.17385E-01     847   0.13819E-01   0.40529E-01 0.37188E-01 
c  k            0.15139E-01     143   0.17447E-03   0.70250E-05 0.17020E+01 
c  epsilon      0.84634E+02     128   0.20327E-03   0.16082E+03 0.48976E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011601                             7
a  epsilon                -0.34604                            16
a  Local Time Step      4.2278e-08                        281595


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9197          3.5475         0.35708        0.081314
v  Velocity[Y]             -3.5075           5.251         0.24965         0.19242
v  Velocity[Z]             -6.1005          3.5939        -0.19732     -0.00055864
v  ǁVelocityǁ           0.00035597          6.7429          1.2219          1.5758
v  Pressure                -935.77           14660          9632.3          7927.2
v  k                    8.2425e-10         0.35959       0.0042635       0.0079915
v  epsilon              5.9613e-05          5474.5          10.626           3.861
v  TurbVisc             4.0701e-14          0.1418      0.00048483       0.0064213
v  CourantNb              0.022262           50082           70.91          17.176
v  FourierNb               0.22186      2.3653e+06          217.37          2.7604
v  total_pressure       4.9906e+05      5.1466e+05      5.0963e+05      5.0793e+05
v  Local Time Step            0.01        0.070228        0.010003        0.010011


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7316      2.3867e+06          288.28          19.936


 TIME FOR THE TIME STEP              153:        0.13854E+03

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


 INSTANT    0.154000000E+02   TIME STEP NUMBER  c  Velocity[Z]                                      0.39193E-01 
c  Pressure     0.17385E-01     847   0.13819E-01   0.40529E-01 0.37188E-01 
c  k            0.15139E-01     143   0.17447E-03   0.70250E-05 0.17020E+01 
c  epsilon      0.84634E+02     128   0.20327E-03   0.16082E+03 0.48976E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011601                             7
a  epsilon                -0.34604                            16
a  Local Time Step      4.2278e-08                        281595


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9197          3.5475         0.35708        0.081314
v  Velocity[Y]             -3.5075           5.251         0.24965         0.19242
v  Velocity[Z]             -6.1005          3.5939        -0.19732     -0.00055864
v  ǁVelocityǁ           0.00035597          6.7429          1.2219          1.5758
v  Pressure                -935.77           14660          9632.3          7927.2
v  k                    8.2425e-10         0.35959       0.0042635       0.0079915
v  epsilon              5.9613e-05          5474.5          10.626           3.861
v  TurbVisc             4.0701e-14          0.1418      0.00048483       0.0064213
v  CourantNb              0.022262           50082           70.91          17.176
v  FourierNb               0.22186      2.3653e+06          217.37          2.7604
v  total_pressure       4.9906e+05      5.1466e+05      5.0963e+05      5.0793e+05
v  Local Time Step            0.01        0.070228        0.010003        0.010011


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7316      2.3867e+06          288.28          19.936


 TIME FOR THE TIME STEP              153:        0.13881E+03

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


 INSTANT    0.154000000E+02   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        -0.277338179E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640997E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12491E+01 0.13895E+01
   Friction velocity        uet   :  0.11973E-01 0.11996E+02
   Friction velocity        uk    :  0.11939E-01 0.11996E+02
   Dimensionless distance   yplus :  0.15307E-02 0.85540E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2468
   Nb of faces within the viscous sub-layer     :      28934
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42692E+00     333   0.15476E+00   0.95721E-01 0.18683E+01 
c  Velocity[X]                                      0.25693E-01 
c  Velocity[Y]                                      0.34236E-01 
c  Velocity[Z]                                      0.35792E-01 
c  Pressure     0.16884E-01     864   0.13345E-01   0.39381E-01 0.30944E-01 
c  k            0.15145E-01     148   0.17594E-03   0.68928E-05 0.16859E+01 
c  epsilon      0.85648E+02     230   0.20433E-03   0.16373E+03 0.49321E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011322                             7
a  epsilon                -0.31927                            18
a  Local Time Step      4.2278e-08                    Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12478E+01 0.13830E+01
   Friction velocity        uet   :  0.93351E-02 0.11136E+02
   Friction velocity        uk    :  0.93324E-02 0.11136E+02
   Dimensionless distance   yplus :  0.14210E-02 0.85535E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2461
   Nb of faces within the viscous sub-layer     :      28937
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42717E+00     326   0.15602E+00   0.95706E-01 0.18681E+01 
c  Velocity[X]                                      0.25577E-01 
c  Velocity[Y]                                      0.34754E-01 
c  Velocity[Z]                                      0.35375E-01 
c  Pressure     0.16537E-01     940   0.12809E-01   0.38541E-01 0.59106E-01 
c  k            0.15136E-01     144   0.18012E-03   0.91482E-05 0.19427E+01 
c  epsilon      0.84717E+02     137   0.19127E-03   0.18721E+03 0.52805E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012032                            10
a  epsilon                -0.32525                            19
a  Local Time Step      4.2278e-08                        281593


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12478E+01 0.13830E+01
   Friction velocity        uet   :  0.93351E-02 0.11136E+02
   Friction velocity        uk    :  0.93324E-02 0.11136E+02
   Dimensionless distance   yplus :  0.14210E-02 0.85535E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2461
   Nb of faces within the viscous sub-layer     :      28937
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42717E+00     326   0.15602E+00   0.95706E-01 0.18681E+01 
c  Velocity[X]                                      0.25577E-01 
c  Velocity[Y]                                      0.34754E-01 
c  Velocity[Z]                                      0.35375E-01 
c  Pressure     0.16537E-01     940   0.12809E-01   0.38541E-01 0.59106E-01 
c  k            0.15136E-01     144   0.18012E-03   0.91482E-05 0.19427E+01 
c  epsilon      0.84717E+02     137   0.19127E-03   0.18721E+03 0.52805E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012032                            10
a  epsilon                -0.32525                            19
a  Local Time Step      4.2278e-08                        281593


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8675          3.5622         0.35683        0.081434
v  Velocity[Y]             -3.5123          5.2165         0.24983         0.19233
v  Velocity[Z]             -6.0891          3.6196        -0.19735     -0.00054694
v  ǁVelocityǁ           0.00061105          6.7361          1.2216          1.5756
v  Pressure                -924.46           14652          9622.6          7920.2
v  k                    6.8611e-09           0.361       0.0042681       0.0079868
v  epsilon              6.0776e-05          5517.5          10.653          3.8613
v  TurbVisc             4.8943e-14          0.1418        0.000485       0.0064198
v  CourantNb               0.01098           47491          70.912          17.172
v  FourierNb                0.2218      2.3653e+06          217.37          2.7604
v  total_pressure       4.9908e+05      5.1465e+05      5.0962e+05      5.0792e+05
v  Local Time Step            0.01         0.05753        0.010003        0.010011


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7208      2.3875e+06          288.29          19.933


 TIME FOR THE TIME STEP              155:        0.14227E+03

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


 INSTANT    0.156000000E+02   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        -0.207668130E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640988E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12454E+01 0.13932E+01
   Friction velocity        uet   :  0.16510E-01 0.11695E+02
   Friction velocity        uk    :  0.16506E-01 0.11695E+02
   Dimensionless distance   yplus :  0.39208E-03 0.85687E+01
   ------------------------------------------------------
   Nb of reversv  FourierNb               0.22179      2.3653e+06          217.37          2.7606
v  total_pressure       4.9908e+05      5.1465e+05      5.0962e+05      5.0792e+05
v  Local Time Step            0.01        0.063283        0.010003        0.010011


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7051      2.3886e+06          288.25          19.933


 TIME FOR THE TIME STEP              156:        0.14587E+03

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


 INSTANT    0.157000000E+02   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        -0.746730259E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699641002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12490E+01 0.13826E+01
   Friction velocity        uet   :  0.14450E-01 0.11386E+02
   Friction velocity        uk    :  0.14447E-01 0.11386E+02
   Dimensionless distance   yplus :  0.13278E-02 0.85771E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2454
   Nb of faces within the viscous sub-layer     :      28934
   Total number of wall faces                   :      41000
-----------------------------------------v  FourierNb               0.22179      2.3653e+06          217.37          2.7606
v  total_pressure       4.9908e+05      5.1465e+05      5.0962e+05      5.0792e+05
v  Local Time Step            0.01        0.063283        0.010003        0.010011


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7051      2.3886e+06          288.25          19.933


 TIME FOR THE TIME STEP              156:        0.13974E+03

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


 INSTANT    0.157000000E+02   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        -0.746730259E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699641002E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12490E+01 0.13826E+01
   Friction velocity        uet   :  0.14450E-01 0.11386E+02
   Friction velocity        uk    :  0.14447E-01 0.11386E+02
   Dimensionless distance   yplus :  0.13278E-02 0.85771E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2454
   Nb of faces within the viscous sub-layer     :      28934
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42714E+00     323   0.15375E+00   0.92948E-01 0.18411E+01 
c  Velocity[X]                                      0.25744E-01 
c  Velocity[Y]                                      0.33670E-01 
c  Velocity[Z]                                      0.33534E-01 
c  Pressure     0.16323E-01     865   0.12488E-01   0.38042E-01 0.35981E-01 
c  k            0.15132E-01     135   0.18510E-03   0.98109E-05 0.20124E+01 
c  epsilon      0.84766E+02     146   0.21441E-03   0.25697E+03 0.61841E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011051                             8
a  epsilon                -0.30622                            13
a  Local Time Step      4.2278e-08                        281593


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8619          3.5711         0.35654         0.08148
v  Velocity[Y]              -3.505            5.23          0.2497         0.19228
v  Velocity[Z]             -6.0742          3.6111        -0.19749     -0.00056723
v  ǁVelocityǁ           0.00036512          6.7248          1.2215          1.5754
v  Pressure                -921.97           14647          9616.5          7915.6
v  k                    6.9471e-09         0.35894        0.004266       0.0079802
v  epsilon              6.1081e-05          5467.8          10.655          3.8569
v  TurbVisc             5.0316e-14          0.1418      0.00048464       0.0064187
v  CourantNb              0.030385           47922          70.855          17.168
v  FourierNb               0.22178      2.3653e+06          217.37          2.7603
v  total_pressure       4.9908e+05      5.1465e+05      5.0962e+05      5.0792e+05
v  Local Time Step            0.01        0.062185        0.010003        0.010011


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7143      2.3891e+06          288.23          19.928


 TIME FOR THE TIME STEP              157:        0.14086E+03

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


 INSTANT    0.158000000E+02   TIME STEP NUMBER             158
 ============================================================= 




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

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00029867                            15
a  epsilon                -0.33454                            24
a  Local Time Step      4.2278e-08                        281606


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8657           3.578         0.35663         0.08152
v  Velocity[Y]             -3.4808           5.254         0.25009          0.1923
v  Velocity[Z]             -6.1125           3.622        -0.19704      -0.0005917
v  ǁVelocityǁ           0.00071942          6.7659          1.2215          1.5753
v  Pressure                -918.41           14649          9618.6          7917.2
v  k                    6.9075e-09         0.35508       0.0042693       0.0079794
v  epsilon              6.1254e-05          5386.1          10.672          3.8606
v  TurbVisc             4.9469e-14          0.1418      0.00048461        0.006418
v  CourantNb              0.011021           46943          70.881          17.169
v  FourierNb               0.22177      2.3653e+06          217.37          2.7603
v  total_pressure       4.9908e+05      5.1465e+05      5.0962e+05      5.0792e+05
v  Local Time Step            0.01        0.068404        0.010003        0.010011


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7102      2.3873e+06          288.26          19.929


 TIME FOR THE TIME STEP              158:        0.14802E+03

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


 INSTANT    0.159000000E+02   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         0.448375668E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640656E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12545E+01 0.13854E+01
   Friction velocity        uet   :  0.14693E-01 0.10481E+02
   Friction velocity        uk    :  0.14688E-01 0.10481E+02
   Dimensionless distance   yplus :  0.13374E-02 0.85948E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2452
   Nb of faces within the viscous sub-layer     :      28936
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42758E+00     321   0.15182E+00   0.93109E-01 0.18424E+01 
c  Velocity[X]                                      0.25913E-01 
c  Velocity[Y]                                      0.33620E-01 
c  Velocity[Z]                                      0.33576E-01 
c  Pressure     0.15848E-01     830   0.12131E-01   0.36898E-01 0.28119E-01 
c  k            0.15131E-01     138   0.19800E-03   0.88125E-05 0.19075E+01 
c  epsilon      0.85277E+02     139   0.30390E-03   0.36395E+03 0.73436E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00018581                            18
a  epsilon                 -10.642                            29
a  Local Time Step      4.2278e-08                        281599


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9618          3.5695         0.35666        0.081538
v  Velocity[Y]             -3.4987          5.2172         0.24978         0.19233
v  Velocity[Z]             -6.1292          3.5901        -0.19676       -0.000621
v  ǁVelocityǁ           0.00059547          6.7901          1.2213          1.5753
v  Pressure                   -919           14648            9616          7915.5
v  k                    6.7629e-09         0.36523       0.0042653       0.0079756
v  epsilon              6.1352e-05          5606.7          10.671          3.8562
v  TurbVisc              4.919e-14          0.1418      0.00048432       0.0064172
v  CourantNb               0.04123           46817          70.874          17.167
v  FourierNb               0.22176      2.3653e+06          217.37          2.7604
v  total_pressure       4.9908e+05      5.1465e+05      5.0962e+05      5.0792e+05
v  Local Time Step            0.01        0.063773        0.010003        0.010011


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6839      2.3885e+06          288.25          19.927


 TIME FOR THE TIME STEP              159:        0.14101E+03

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


 INSTANT    0.160000000E+02   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        -0.731385568E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699641003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           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+01 0.13974E+01
   Friction velocity        uet   :  0.15211E-01 0.10960E+02
   Friction velocity        uk    :  0.15208E-01 0.10960E+02
   Dimensionless distance   yplus :  0.12023E-02 0.86059E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2452
   Nb of faces within the viscous sub-layer     :      28931
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42787E+00     324   0.15121E+00   0.92813E-01 0.18396E+01 
c  Velocity[X]                                      0.25902E-01 
c  Velocity[Y]                                      0.33747E-01 
c  Velocity[Z]                                      0.33164E-01 
c  Pressure     0.15969E-01     734   0.12552E-01   0.37205E-01 0.27292E-01 
c  k            0.15138E-01     131   0.17923E-03   0.60560E-05 0.15812E+01 
c  epsilon      0.86127E+02     158   0.23304E-03   0.16727E+03 0.49896E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00023626                            15
a  epsilon                -0.35087                            20
a  Local Time Step      4.2278e-08                        281601


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8199          3.5487         0.35689        0.081555
v  Velocity[Y]              -3.483          5.2719         0.24981         0.19234
v  Velocity[Z]             -6.0857          3.6213        -0.19624     -0.00059761
v  ǁVelocityǁ           0.00062719          6.7506           1.221          1.5751
v  Pressure                 -923.5           14647          9615.4          7914.9
v  k                    6.7034e-09          0.3532       0.0042608       0.0079746
v  epsilon              6.1696e-05          5334.3          10.614          3.8547
v  TurbVisc             4.8111e-14          0.1418       0.0004841       0.0064167
v  CourantNb              0.002031           45831          70.881          17.165
v  FourierNb               0.22174      2.3653e+06          217.37          2.7602
v  total_pressure       4.9908e+05      5.1465e+05      5.0962e+05      5.0791e+05
v  Local Time Step            0.01         0.07015        0.010003        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6949      2.3893e+06          288.26          19.925


 TIME FOR THE TIME STEP              160:        0.13613E+03

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


 INSTANT    0.161000000E+02   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        -0.342338224E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699641008E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           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+01 0.13838E+01
   Friction velocity        uet   :  0.72983E-02 0.10023E+02
   Friction velocity        uk    :  0.72950E-02 0.10023E+02
   Dimensionless distance   yplus :  0.12790E-02 0.86058E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2451
   Nb of faces within the viscous sub-layer     :      28938
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42802E+00     329   0.15380E+00   0.92226E-01 0.18336E+01 
c  Velocity[X]                                      0.27291E-01 
c  Velocity[Y]                                      0.32829E-01 
c  Velocity[Z]                                      0.32105E-01 
c  Pressure     0.16155E-01     701   0.12757E-01   0.37624E-01 0.28688E-01 
c  k            0.15123E-01     145   0.20978E-03   0.89118E-05 0.19185E+01 
c  epsilon      0.84960E+02     128   0.28727E-03   0.28824E+03 0.65536E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021129                            17
a  epsilon                 -5.7594                            22
a  Local Time Step      4.2278e-08                        281598


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9459          3.5555         0.35663          0.0815
v  Velocity[Y]             -3.5109          5.1945         0.25008         0.19231
v  Velocity[Z]             -6.1031          3.6181        -0.19584     -0.00058699
v  ǁVelocityǁ           0.00065689          6.7614          1.2205          1.5751
v  Pressure                -941.17           14649          9616.4            7915
v  k                     6.007e-09         0.35839       0.0042631       0.0079725
v  epsilon              6.2067e-05          5455.5          10.657           3.853
v  TurbVisc             4.7852e-14          0.1418      0.00048434       0.0064164
v  CourantNb               0.01708           46087          70.879          17.161
v  FourierNb               0.22174      2.3653e+06          217.37          2.7598
v  total_pressure       4.9906e+05      5.1465e+05      5.0962e+05      5.0792e+05
v  Local Time Step            0.01        0.068432        0.010003        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7165      2.3891e+06          288.25          19.921


 TIME FOR THE TIME STEP              161:        0.13299E+03

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


 INSTANT    0.162000000E+02   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        -0.396516317E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640659E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12528E+01 0.13947E+01
   Friction velocity        uet   :  0.94836E-02 0.90381E+01
   Friction velocity        uk    :  0.94801E-02 0.90381E+01
   Dimensionless distance   yplus :  0.11533E-02 0.86112E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2449
   Nb of faces within the viscous sub-layer     :      28932
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42817E+00     325   0.15693E+00   0.96685E-01 0.18772E+01 
c  Velocity[X]                                      0.27997E-01 
c  Velocity[Y]                                      0.34622E-01 
c  Velocity[Z]                                      0.34066E-01 
c  Pressure     0.17027E-01     852   0.13504E-01   0.39648E-01 0.40216E-01 
c  k            0.15127E-01     137   0.19605E-03   0.84691E-05 0.18701E+01 
c  epsilon      0.86046E+02     146   0.26950E-03   0.28324E+03 0.64842E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00022399                            16
a  epsilon                -0.32512                            19
a  Local Time Step      4.2278e-08                        281601


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8324          3.5604         0.35699        0.081508
v  Velocity[Y]             -3.4965          5.2352         0.25007         0.19229
v  Velocity[Z]             -6.0779           3.595        -0.19581     -0.00057425
v  ǁVelocityǁ           0.00054607           6.728           1.221          1.5751
v  Pressure                -963.46           14652          9620.1          7917.2
v  k                    6.0407e-09         0.35993        0.004261        0.007972
v  epsilon              6.2311e-05          5494.9          10.631          3.8534
v  TurbVisc             4.1745e-14          0.1418      0.00048386       0.0064162
v  CourantNb              0.017089           47167          70.808          17.159
v  FourierNb               0.22174      2.3653e+06          217.37          2.7606
v  total_pressure       4.9904e+05      5.1465e+05      5.0962e+05      5.0792e+05
v  Local Time Step            0.01        0.075275        0.010003        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6781      2.3869e+06          288.18          19.919


 TIME FOR THE TIME STEP              162:        0.14218E+03

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


 INSTANT    0.163000000E+02   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        -0.106062070E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640650E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12352E+01 0.13864E+01
   Friction velocity        uet   :  0.16972E-01 0.10408E+02
   Friction velocity        uk    :  0.16792E-01 0.10408E+02
   Dimensionless distance   yplus :  0.13280E-02 0.86087E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2454
   Nb of faces within the viscous sub-layer     :      28941
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42809E+00     320   0.15747E+00   0.97016E-01 0.18805E+01 
c  Velocity[X]                                      0.28355E-01 
c  Velocity[Y]                                      0.33658E-01 
c  Velocity[Z]                                      0.35003E-01 
c  Pressure     0.17371E-01     635   0.13802E-01   0.40466E-01 0.32958E-01 
c  k            0.15138E-01     128   0.17172E-03   0.64522E-05 0.16321E+01 
c  epsilon      0.85350E+02     124   0.21630E-03   0.13705E+03 0.45114E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021295                            17
a  epsilon                 -6.2639                            26
a  Local Time Step      4.2278e-08                        281600


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9526          3.5503         0.35685        0.081552
v  Velocity[Y]             -3.5059          5.2174         0.24994         0.19228
v  Velocity[Z]             -6.0751          3.6156        -0.19551     -0.00058561
v  ǁVelocityǁ           0.00039354          6.7265          1.2208           1.575
v  Pressure                -991.95           14653          9619.9          7916.8
v  k                     6.327e-09         0.35719       0.0042612       0.0079713
v  epsilon              6.2204e-05          5430.6           10.64          3.8545
v  TurbVisc             4.4535e-14          0.1418      0.00048374       0.0064162
v  CourantNb              0.019783           46172          70.868          17.161
v  FourierNb               0.22175      2.3653e+06          217.37          2.7604
v  total_pressure       4.9901e+05      5.1465e+05      5.0962e+05      5.0792e+05
v  Local Time Step            0.01        0.058342        0.010003        0.010011


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier            1.67      2.3869e+06          288.24          19.921


 TIME FOR THE TIME STEP              163:        0.12955E+03

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


 INSTANT    0.164000000E+02   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        -0.153566413E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640999E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12402E+01 0.13964E+01
   Friction velocity        uet   :  0.10085E-01 0.10192E+02
   Friction velocity        uk    :  0.10069E-01 0.10192E+02
   Dimensionless distance   yplus :  0.13005E-02 0.86164E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2447
   Nb of faces within the viscous sub-layer     :      28929
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42796E+00     326   0.15512E+00   0.97062E-01 0.18809E+01 
c  Velocity[X]                                      0.28839E-01 
c  Velocity[Y]                                      0.33555E-01 
c  Velocity[Z]                                      0.34668E-01 
c  Pressure     0.17309E-01     902   0.13875E-01   0.40351E-01 0.48882E-01 
c  k            0.15129E-01     144   0.17480E-03   0.70645E-05 0.17082E+01 
c  epsilon      0.86029E+02     174   0.29055E-03   0.21337E+03 0.56312E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021647                            17
a  epsilon                -0.31445                            20
a  Local Time Step      4.2278e-08                        281610


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8196          3.5711         0.35665        0.081548
v  Velocity[Y]             -3.4964          5.2184         0.25019         0.19227
v  Velocity[Z]             -6.0864          3.6174        -0.19514     -0.00051899
v  ǁVelocityǁ           0.00028404           6.736          1.2206          1.5748
v  Pressure                -1016.4           14658          9624.1          7919.8
v  k                    6.3032e-09         0.35822       0.0042586       0.0079695
v  epsilon              6.1923e-05          5451.2          10.626          3.8514
v  TurbVisc             4.5838e-14          0.1418      0.00048393       0.0064161
v  CourantNb              0.046387           45359          70.859          17.157
v  FourierNb               0.22176      2.3653e+06          217.37            2.76
v  total_pressure       4.9898e+05      5.1466e+05      5.0962e+05      5.0792e+05
v  Local Time Step            0.01        0.064176        0.010003        0.010011


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6803       2.387e+06          288.23          19.917


 TIME FOR THE TIME STEP              164:        0.14826E+03

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


 INSTANT    0.165000000E+02   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        -0.527840094E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640667E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12452E+01 0.13980E+01
   Friction velocity        uet   :  0.77076E-02 0.90361E+01
   Friction velocity        uk    :  0.77055E-02 0.90361E+01
   Dimensionless distance   yplus :  0.11530E-02 0.86140E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2445
   Nb of faces within the viscous sub-layer     :      28943
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42814E+00     321   0.15719E+00   0.95859E-01 0.18693E+01 
c  Velocity[X]                                      0.27980E-01 
c  Velocity[Y]                                      0.33103E-01 
c  Velocity[Z]                                      0.34776E-01 
c  Pressure     0.16666E-01     943   0.13098E-01   0.38860E-01 0.60909E-01 
c  k            0.15134E-01     134   0.19233E-03   0.10382E-04 0.20707E+01 
c  epsilon      0.85865E+02     124   0.25319E-03   0.29061E+03 0.65741E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021437                            17
a  epsilon                 -6.2588                            22
a  Local Time Step      4.2278e-08                        281597


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9433          3.5487         0.35649        0.081494
v  Velocity[Y]              -3.514          5.2192         0.24996         0.19221
v  Velocity[Z]             -6.0759          3.5814        -0.19486     -0.00053545
v  ǁVelocityǁ           0.00027858          6.7229          1.2204          1.5747
v  Pressure                -1034.4           14665          9630.2          7924.4
v  k                    6.2919e-09         0.35713       0.0042575       0.0079695
v  epsilon              6.1649e-05          5432.4          10.635          3.8516
v  TurbVisc             4.5634e-14          0.1418      0.00048365       0.0064161
v  CourantNb              0.016999           44845          70.829          17.155
v  FourierNb               0.22177      2.3653e+06          217.37          2.7601
v  total_pressure       4.9897e+05      5.1467e+05      5.0963e+05      5.0792e+05
v  Local Time Step            0.01        0.068712        0.010003        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.692      2.3879e+06           288.2          19.915


 TIME FOR THE TIME STEP              165:        0.14523E+03

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


 INSTANT    0.166000000E+02   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        -0.213468303E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640652E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12160E+01 0.13982E+01
   Friction velocity        uet   :  0.10633E-01 0.91570E+01
   Friction velocity        uk    :  0.10630E-01 0.91570E+01
   Dimensionless distance   yplus :  0.11489E-02 0.86194E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2445
   Nb of faces within the viscous sub-layer     :      28934
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42816E+00     329   0.15446E+00   0.96312E-01 0.18735E+01 
c  Velocity[X]                                      0.27040E-01 
c  Velocity[Y]                                      0.33148E-01 
c  Velocity[Z]                                      0.36124E-01 
c  Pressure     0.16822E-01     901   0.13043E-01   0.39235E-01 0.42691E-01 
c  k            0.15131E-01     131   0.20291E-03   0.74207E-05 0.17504E+01 
c  epsilon      0.86144E+02     137   0.27999E-03   0.22841E+03 0.58183E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00022157                            14
a  epsilon                -0.30798                            19
a  Local Time Step      4.2278e-08                        281597


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -1.914          3.5577         0.35624        0.081457
v  Velocity[Y]              -3.495          5.2769         0.25008         0.19218
v  Velocity[Z]             -6.0489          3.6218        -0.19532     -0.00051565
v  ǁVelocityǁ           0.00091274          6.6925          1.2207          1.5747
v  Pressure                -1052.1           14670          9634.2          7927.1
v  k                    6.2496e-09         0.35963       0.0042584       0.0079698
v  epsilon              6.1335e-05          5481.9          10.639          3.8528
v  TurbVisc             4.5279e-14          0.1418      0.00048319       0.0064163
v  CourantNb              0.019932           46086          70.803          17.153
v  FourierNb               0.22179      2.3653e+06          217.37          2.7604
v  total_pressure       4.9895e+05      5.1467e+05      5.0963e+05      5.0793e+05
v  Local Time Step            0.01        0.075583        0.010003        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6898      2.3873e+06          288.18          19.913


 TIME FOR THE TIME STEP              166:        0.14261E+03

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


 INSTANT    0.167000000E+02   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        -0.427466486E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640669E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12253E+01 0.14001E+01
   Friction velocity        uet   :  0.71479E-02 0.97771E+01
   Friction velocity        uk    :  0.71458E-02 0.97771E+01
   Dimensionless distance   yplus :  0.12476E-02 0.86214E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2450
   Nb of faces within the viscous sub-layer     :      28937
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42812E+00     323   0.15388E+00   0.93607E-01 0.18469E+01 
c  Velocity[X]                                      0.27100E-01 
c  Velocity[Y]                                      0.32281E-01 
c  Velocity[Z]                                      0.34226E-01 
c  Pressure     0.16433E-01     919   0.12500E-01   0.38349E-01 0.44533E-01 
c  k            0.15137E-01     145   0.18480E-03   0.60697E-05 0.15768E+01 
c  epsilon      0.86190E+02     124   0.22363E-03   0.12868E+03 0.43606E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00016383                            18
a  epsilon                  -6.242                            25
a  Local Time Step      4.2278e-08                        281600


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9859          3.5551         0.35654        0.081509
v  Velocity[Y]             -3.5095          5.1979         0.25036         0.19219
v  Velocity[Z]             -6.0506          3.6257        -0.19561     -0.00052693
v  ǁVelocityǁ            0.0004971          6.6978          1.2214          1.5747
v  Pressure                  -1066           14676          9638.7            7930
v  k                    6.2211e-09         0.35585       0.0042619       0.0079706
v  epsilon              6.1153e-05          5406.5          10.651          3.8535
v  TurbVisc             4.4954e-14          0.1418      0.00048325       0.0064165
v  CourantNb              0.036719           45215          70.822          17.154
v  FourierNb               0.22182      2.3653e+06          217.37          2.7601
v  total_pressure       4.9893e+05      5.1468e+05      5.0964e+05      5.0793e+05
v  Local Time Step            0.01        0.053776        0.010003        0.010011


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7028      2.3901e+06           288.2          19.914


 TIME FOR THE TIME STEP              167:        0.14200E+03

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


 INSTANT    0.168000000E+02   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        -0.732598572E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640642E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12261E+01 0.13988E+01
   Friction velocity        uet   :  0.10147E-01 0.91806E+01
   Friction velocity        uk    :  0.10145E-01 0.91806E+01
   Dimensionless distance   yplus :  0.11715E-02 0.86198E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2448
   Nb of faces within the viscous sub-layer     :      28939
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42847E+00     335   0.15533E+00   0.93332E-01 0.18441E+01 
c  Velocity[X]                                      0.26118E-01 
c  Velocity[Y]                                      0.33099E-01 
c  Velocity[Z]                                      0.34115E-01 
c  Pressure     0.16253E-01     813   0.12251E-01   0.37947E-01 0.27405E-01 
c  k            0.15139E-01     138   0.17444E-03   0.47317E-05 0.13976E+01 
c  epsilon      0.86337E+02     152   0.24032E-03   0.10723E+03 0.39804E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021921                            16
a  epsilon                -0.30145                            20
a  Local Time Step      4.2278e-08                        281598


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8447          3.5331         0.35654        0.081481
v  Velocity[Y]             -3.4928          5.2595         0.25018         0.19213
v  Velocity[Z]             -6.0734          3.5908        -0.19547     -0.00053946
v  ǁVelocityǁ           0.00075859          6.7266          1.2214          1.5747
v  Pressure                -1076.6           14678          9640.4          7931.2
v  k                    6.2392e-09         0.35866       0.0042596       0.0079697
v  epsilon              6.1215e-05          5462.1          10.651          3.8548
v  TurbVisc             4.4562e-14          0.1418       0.0004832       0.0064167
v  CourantNb              0.029158           45384          70.884          17.154
v  FourierNb               0.22184      2.3653e+06          217.37          2.7604
v  total_pressure       4.9892e+05      5.1468e+05      5.0964e+05      5.0793e+05
v  Local Time Step            0.01        0.059154        0.010003        0.010011


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6611      2.3894e+06          288.26          19.915


 TIME FOR THE TIME STEP              168:        0.14122E+03

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


 INSTANT    0.169000000E+02   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        -0.249716899E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640635E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12116E+01 0.14014E+01
   Friction velocity        uet   :  0.13387E-01 0.83749E+01
   Friction velocity        uk    :  0.13384E-01 0.83749E+01
   Dimensionless distance   yplus :  0.10686E-02 0.86092E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2449
   Nb of faces within the viscous sub-layer     :      28943
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42830E+00     314   0.16039E+00   0.94362E-01 0.18542E+01 
c  Velocity[X]                                      0.26801E-01 
c  Velocity[Y]                                      0.33746E-01 
c  Velocity[Z]                                      0.33815E-01 
c  Pressure     0.16310E-01     852   0.12139E-01   0.38082E-01 0.29969E-01 
c  k            0.15143E-01     136   0.17114E-03   0.49179E-05 0.14248E+01 
c  epsilon      0.86193E+02     120   0.21605E-03   0.11805E+03 0.41845E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00022417                            18
a  epsilon                 -6.5093                            25
a  Local Time Step      4.2278e-08                        281589


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9764           3.528         0.35626        0.081494
v  Velocity[Y]             -3.5036          5.2281         0.25034          0.1921
v  Velocity[Z]             -6.0224          3.6157        -0.19606     -0.00050269
v  ǁVelocityǁ           0.00036449          6.6711          1.2216          1.5747
v  Pressure                -1085.8           14681          9642.9          7932.7
v  k                    6.3312e-09          0.3588       0.0042612       0.0079713
v  epsilon              6.1499e-05            5462          10.661          3.8556
v  TurbVisc             4.5031e-14          0.1418      0.00048291       0.0064167
v  CourantNb              0.024424           45660           70.87          17.154
v  FourierNb               0.22186      2.3653e+06          217.37            2.76
v  total_pressure       4.9891e+05      5.1468e+05      5.0964e+05      5.0793e+05
v  Local Time Step            0.01         0.06507        0.010004        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6763      2.3888e+06          288.24          19.914


 TIME FOR THE TIME STEP              169:        0.13777E+03

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


 INSTANT    0.170000000E+02   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        -0.566451646E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640641E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12183E+01 0.14005E+01
   Friction velocity        uet   :  0.12815E-01 0.86857E+01
   Friction velocity        uk    :  0.12811E-01 0.86857E+01
   Dimensionless distance   yplus :  0.11083E-02 0.86366E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2450
   Nb of faces within the viscous sub-layer     :      28936
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42825E+00     321   0.16030E+00   0.10022E+00 0.19110E+01 
c  Velocity[X]                                      0.27890E-01 
c  Velocity[Y]                                      0.35904E-01 
c  Velocity[Z]                                      0.36429E-01 
c  Pressure     0.16744E-01     940   0.12510E-01   0.39117E-01 0.50204E-01 
c  k            0.15136E-01     148   0.18060E-03   0.60427E-05 0.15790E+01 
c  epsilon      0.86329E+02     160   0.23771E-03   0.18811E+03 0.52735E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021962                            15
a  epsilon                -0.30091                            25
a  Local Time Step      4.2278e-08                        281597


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9639          3.5389         0.35636        0.081453
v  Velocity[Y]             -3.4963          5.2593         0.25078         0.19201
v  Velocity[Z]             -6.0666          3.6156        -0.19601     -0.00041307
v  ǁVelocityǁ           0.00064538          6.7212          1.2221          1.5745
v  Pressure                -1091.2           14687          9648.1          7936.4
v  k                    7.6102e-09         0.35499       0.0042685       0.0079732
v  epsilon              6.1994e-05            5381          10.679          3.8582
v  TurbVisc             4.5397e-14          0.1418      0.00048267       0.0064171
v  CourantNb              0.016694           45239          70.885          17.154
v  FourierNb               0.22188      2.3653e+06          217.37          2.7604
v  total_pressure       4.9891e+05      5.1469e+05      5.0965e+05      5.0794e+05
v  Local Time Step            0.01        0.071576        0.010004        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6567      2.3882e+06          288.26          19.914


 TIME FOR THE TIME STEP              170:        0.14484E+03

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


 INSTANT    0.171000000E+02   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        -0.261881603E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640652E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11977E+01 0.13988E+01
   Friction velocity        uet   :  0.14497E-01 0.76369E+01
   Friction velocity        uk    :  0.14494E-01 0.76369E+01
   Dimensionless distance   yplus :  0.95325E-03 0.86021E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2457
   Nb of faces within the viscous sub-layer     :      28932
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42798E+00     334   0.15710E+00   0.96139E-01 0.18716E+01 
c  Velocity[X]                                      0.25538E-01 
c  Velocity[Y]                                      0.33461E-01 
c  Velocity[Z]                                      0.37140E-01 
c  Pressure     0.16262E-01    1048   0.11989E-01   0.37973E-01 0.96557E-01 
c  k            0.15144E-01     144   0.19993E-03   0.56819E-05 0.15314E+01 
c  epsilon      0.86182E+02     120   0.30781E-03   0.23337E+03 0.58699E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021613                            20
a  epsilon                -0.33314                            22
a  Local Time Step      4.2278e-08                        281593


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9008          3.5166         0.35617        0.081395
v  Velocity[Y]             -3.5186          5.2392          0.2504         0.19194
v  Velocity[Z]             -5.9992          3.5878        -0.19627     -0.00047622
v  ǁVelocityǁ           0.00028365          6.6426          1.2219          1.5746
v  Pressure                -1087.6           14699          9659.5          7944.8
v  k                    5.5163e-09         0.36256       0.0042662       0.0079738
v  epsilon              6.2423e-05          5558.7          10.707          3.8584
v  TurbVisc             5.2867e-14          0.1418      0.00048255       0.0064173
v  CourantNb              0.016686           46240          70.917          17.155
v  FourierNb               0.22189      2.3653e+06          217.37          2.7598
v  total_pressure       4.9891e+05       5.147e+05      5.0966e+05      5.0794e+05
v  Local Time Step            0.01        0.071325        0.010003        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6362       2.387e+06          288.29          19.915


 TIME FOR THE TIME STEP              171:        0.14936E+03

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


 INSTANT    0.172000000E+02   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         0.795395722E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640646E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12041E+01 0.14006E+01
   Friction velocity        uet   :  0.71952E-02 0.77413E+01
   Friction velocity        uk    :  0.71931E-02 0.77413E+01
   Dimensionless distance   yplus :  0.66960E-03 0.86910E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2453
   Nb of faces within the viscous sub-layer     :      28936
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42799E+00     324   0.15560E+00   0.96917E-01 0.18791E+01 
c  Velocity[X]                                      0.24873E-01 
c  Velocity[Y]                                      0.34739E-01 
c  Velocity[Z]                                      0.37306E-01 
c  Pressure     0.15946E-01     744   0.11645E-01   0.37247E-01 0.17487E-01 
c  k            0.15143E-01     136   0.24543E-03   0.78440E-05 0.17989E+01 
c  epsilon      0.86389E+02     148   0.46152E-03   0.57752E+03 0.92152E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00022209                            15
a  epsilon                 -11.068                            23
a  Local Time Step      4.2278e-08                        281593


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -1.899           3.528           0.356        0.081331
v  Velocity[Y]             -3.4915          5.2721         0.25064         0.19187
v  Velocity[Z]             -6.0797          3.6174        -0.19627     -0.00048664
v  ǁVelocityǁ           0.00062123          6.7283          1.2221          1.5745
v  Pressure                -1093.2           14697          9658.5            7944
v  k                     5.691e-09         0.35825       0.0042645       0.0079752
v  epsilon              6.3029e-05          5461.2          10.675          3.8608
v  TurbVisc             3.5798e-14          0.1418      0.00048235       0.0064176
v  CourantNb               0.01629           44189          70.863          17.155
v  FourierNb               0.22191      2.3653e+06          217.37          2.7601
v  total_pressure       4.9891e+05       5.147e+05      5.0966e+05      5.0794e+05
v  Local Time Step            0.01        0.078457        0.010004        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6332       2.384e+06          288.24          19.915


 TIME FOR THE TIME STEP              172:        0.13739E+03

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


 INSTANT    0.173000000E+02   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        -0.374312898E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699641007E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11939E+01 0.14004E+01
   Friction velocity        uet   :  0.10418E-01 0.73516E+01
   Friction velocity        uk    :  0.10330E-01 0.73516E+01
   Dimensionless distance   yplus :  0.83350E-03 0.85986E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2451
   Nb of faces within the viscous sub-layer     :      28940
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42812E+00     320   0.15961E+00   0.94710E-01 0.18574E+01 
c  Velocity[X]                                      0.25752E-01 
c  Velocity[Y]                                      0.32570E-01 
c  Velocity[Z]                                      0.36388E-01 
c  Pressure     0.15578E-01     685   0.11155E-01   0.36401E-01 0.14342E-01 
c  k            0.15139E-01     144   0.22259E-03   0.63629E-05 0.16207E+01 
c  epsilon      0.86170E+02     130   0.36793E-03   0.29735E+03 0.66338E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021942                            20
a  epsilon                -0.35408                            28
a  Local Time Step      4.2278e-08                        281595


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9539          3.5343         0.35588        0.081284
v  Velocity[Y]             -3.5055          5.1666         0.25077         0.19186
v  Velocity[Z]             -5.9922          3.6243        -0.19616     -0.00044899
v  ǁVelocityǁ           0.00030254          6.6373          1.2223          1.5746
v  Pressure                -1098.5           14699            9659          7944.4
v  k                    6.3145e-09         0.35906       0.0042625       0.0079745
v  epsilon              6.3126e-05          5480.1          10.688          3.8572
v  TurbVisc             4.2095e-14          0.1418      0.00048208       0.0064177
v  CourantNb             0.0012142           44796          70.902          17.153
v  FourierNb               0.22193      2.3653e+06          217.37          2.7602
v  total_pressure        4.989e+05       5.147e+05      5.0966e+05      5.0794e+05
v  Local Time Step            0.01        0.055416        0.010003        0.010011


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6603      2.3864e+06          288.28          19.914


 TIME FOR THE TIME STEP              173:        0.13386E+03

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


 INSTANT    0.174000000E+02   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         0.464760791E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640642E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12022E+01 0.14014E+01
   Friction velocity        uet   :  0.88453E-02 0.80356E+01
   Friction velocity        uk    :  0.88443E-02 0.80356E+01
   Dimensionless distance   yplus :  0.82702E-03 0.87127E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2455
   Nb of faces within the viscous sub-layer     :      28937
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42809E+00     324   0.16012E+00   0.99153E-01 0.19008E+01 
c  Velocity[X]                                      0.26956E-01 
c  Velocity[Y]                                      0.35136E-01 
c  Velocity[Z]                                      0.37060E-01 
c  Pressure     0.16098E-01     772   0.11474E-01   0.37604E-01 0.15884E-01 
c  k            0.15149E-01     141   0.17393E-03   0.57221E-05 0.15364E+01 
c  epsilon      0.86495E+02     162   0.21781E-03   0.14975E+03 0.47001E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021916                            14
a  epsilon                 -5.8324                            21
a  Local Time Step      4.2278e-08                        281597


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8427          3.5317         0.35635        0.081252
v  Velocity[Y]             -3.4982          5.2368         0.25075         0.19186
v  Velocity[Z]             -6.0875          3.5851        -0.19604      -0.0003905
v  ǁVelocityǁ           0.00031617          6.7349          1.2227          1.5745
v  Pressure                -1107.8           14698          9657.9          7943.7
v  k                    7.5917e-09          0.3604       0.0042634        0.007976
v  epsilon              6.2877e-05          5506.1          10.671          3.8609
v  TurbVisc             4.5749e-14          0.1418      0.00048169       0.0064177
v  CourantNb              0.037259           44722          70.921          17.155
v  FourierNb               0.22195      2.3653e+06          217.37          2.7597
v  total_pressure       4.9889e+05       5.147e+05      5.0966e+05      5.0794e+05
v  Local Time Step            0.01        0.060958        0.010003        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6477      2.3876e+06           288.3          19.915


 TIME FOR THE TIME STEP              174:        0.14134E+03

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


 INSTANT    0.175000000E+02   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        -0.338587493E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640996E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11921E+01 0.13981E+01
   Friction velocity        uet   :  0.98867E-02 0.74088E+01
   Friction velocity        uk    :  0.98483E-02 0.74088E+01
   Dimensionless distance   yplus :  0.94537E-03 0.86171E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2457
   Nb of faces within the viscous sub-layer     :      28936
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42737E+00     313   0.15448E+00   0.95809E-01 0.18686E+01 
c  Velocity[X]                                      0.24883E-01 
c  Velocity[Y]                                      0.33957E-01 
c  Velocity[Z]                                      0.36969E-01 
c  Pressure     0.15826E-01     827   0.11235E-01   0.36988E-01 0.18133E-01 
c  k            0.15139E-01     134   0.17718E-03   0.53717E-05 0.14889E+01 
c  epsilon      0.86044E+02     130   0.24530E-03   0.13736E+03 0.45050E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00022259                            18
a  epsilon                -0.34042                            25
a  Local Time Step      4.2278e-08                        281603


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9729          3.5211          0.3563        0.081247
v  Velocity[Y]              -3.509          5.2263         0.25067         0.19185
v  Velocity[Z]             -5.9828          3.6065        -0.19618     -0.00039039
v  ǁVelocityǁ           0.00020141          6.6258          1.2225          1.5745
v  Pressure                -1112.1           14700          9659.6          7944.8
v  k                    6.1425e-09         0.36011       0.0042649       0.0079765
v  epsilon              6.2594e-05          5499.7            10.7          3.8587
v  TurbVisc             5.2585e-14          0.1418      0.00048193       0.0064179
v  CourantNb             0.0013875           44696          70.956          17.155
v  FourierNb               0.22195      2.3653e+06          217.37          2.7602
v  total_pressure       4.9889e+05       5.147e+05      5.0966e+05      5.0794e+05
v  Local Time Step            0.01        0.062352        0.010003        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6346      2.3899e+06          288.33          19.915


 TIME FOR THE TIME STEP              175:        0.13761E+03

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


 INSTANT    0.176000000E+02   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        -0.126441442E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640671E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11957E+01 0.14015E+01
   Friction velocity        uet   :  0.98388E-02 0.86027E+01
   Friction velocity        uk    :  0.98382E-02 0.86027E+01
   Dimensionless distance   yplus :  0.97108E-03 0.85966E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2457
   Nb of faces within the viscous sub-layer     :      28928
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42757E+00     317   0.15595E+00   0.92147E-01 0.18324E+01 
c  Velocity[X]                                      0.25177E-01 
c  Velocity[Y]                                      0.32670E-01 
c  Velocity[Z]                                      0.34300E-01 
c  Pressure     0.15198E-01     884   0.10873E-01   0.35517E-01 0.29641E-01 
c  k            0.15143E-01     146   0.19829E-03   0.66615E-05 0.16577E+01 
c  epsilon      0.86339E+02     138   0.22472E-03   0.15522E+03 0.47944E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021678                            17
a  epsilon                 -6.5268                            22
a  Local Time Step      4.2278e-08                        281592


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8324          3.5369         0.35638        0.081254
v  Velocity[Y]             -3.4939          5.1404         0.25121         0.19188
v  Velocity[Z]             -6.0624          3.6167        -0.19654     -0.00037325
v  ǁVelocityǁ           0.00068969          6.7194          1.2232          1.5745
v  Pressure                -1116.9           14703          9662.5          7947.3
v  k                    6.7636e-09         0.35436       0.0042679       0.0079801
v  epsilon              6.2198e-05            5364          10.658          3.8627
v  TurbVisc             4.2505e-14          0.1418       0.0004824       0.0064184
v  CourantNb            7.9748e-05           44973          70.949          17.156
v  FourierNb               0.22196      2.3653e+06          217.37          2.7602
v  total_pressure       4.9888e+05       5.147e+05      5.0966e+05      5.0795e+05
v  Local Time Step            0.01        0.068587        0.010003        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6262      2.3885e+06          288.32          19.916


 TIME FOR THE TIME STEP              176:        0.14269E+03

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


 INSTANT    0.177000000E+02   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        -0.651895886E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640645E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11887E+01 0.14006E+01
   Friction velocity        uet   :  0.12619E-01 0.71244E+01
   Friction velocity        uk    :  0.12583E-01 0.71244E+01
   Dimensionless distance   yplus :  0.90907E-03 0.86172E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2460
   Nb of faces within the viscous sub-layer     :      28924
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42765E+00     321   0.15600E+00   0.90550E-01 0.18163E+01 
c  Velocity[X]                                      0.24979E-01 
c  Velocity[Y]                                      0.31618E-01 
c  Velocity[Z]                                      0.33953E-01 
c  Pressure     0.15250E-01     649   0.10862E-01   0.35646E-01 0.13315E-01 
c  k            0.15146E-01     147   0.22378E-03   0.78627E-05 0.18008E+01 
c  epsilon      0.86309E+02     228   0.25144E-03   0.18350E+03 0.51965E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.000224                            18
a  epsilon                -0.34839                            24
a  Local Time Step      4.2278e-08                        281585


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -1.981          3.5116          0.3564        0.081217
v  Velocity[Y]             -3.5115          5.1079         0.25065         0.19187
v  Velocity[Z]             -5.9906          3.5794        -0.19648     -0.00038599
v  ǁVelocityǁ           0.00031595          6.6358          1.2232          1.5746
v  Pressure                -1123.6           14704          9662.8          7947.7
v  k                    6.7744e-09         0.36166       0.0042759       0.0079813
v  epsilon               6.172e-05          5533.1           10.74           3.866
v  TurbVisc             4.8238e-14          0.1418      0.00048271       0.0064186
v  CourantNb             0.0068273           42653          71.005          17.158
v  FourierNb               0.22198      2.3653e+06          217.38          2.7603
v  total_pressure       4.9888e+05       5.147e+05      5.0966e+05      5.0795e+05
v  Local Time Step            0.01        0.064647        0.010004        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6278      2.3907e+06          288.38          19.918


 TIME FOR THE TIME STEP              177:        0.13489E+03

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


 INSTANT    0.178000000E+02   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        -0.227650869E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640645E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11938E+01 0.14017E+01
   Friction velocity        uet   :  0.75923E-02 0.62808E+01
   Friction velocity        uk    :  0.75520E-02 0.62808E+01
   Dimensionless distance   yplus :  0.70001E-03 0.85941E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2460
   Nb of faces within the viscous sub-layer     :      28933
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42753E+00     313   0.15568E+00   0.91411E-01 0.18250E+01 
c  Velocity[X]                                      0.25161E-01 
c  Velocity[Y]                                      0.31290E-01 
c  Velocity[Z]                                      0.34960E-01 
c  Pressure     0.15299E-01     872   0.10832E-01   0.35771E-01 0.31844E-01 
c  k            0.15156E-01     138   0.18064E-03   0.67853E-05 0.16725E+01 
c  epsilon      0.86564E+02     141   0.22331E-03   0.17481E+03 0.50773E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021736                            20
a  epsilon                 -6.3448                            30
a  Local Time Step      4.2278e-08                        281597


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8619          3.5277         0.35639        0.081186
v  Velocity[Y]             -3.4825          5.1603         0.25038         0.19179
v  Velocity[Z]             -6.0742           3.607        -0.19632      -0.0004168
v  ǁVelocityǁ           0.00058309          6.7253          1.2231          1.5745
v  Pressure                -1129.1           14707          9666.3          7950.4
v  k                    7.0567e-09          0.3584       0.0042649       0.0079821
v  epsilon              6.1421e-05          5472.2          10.662          3.8643
v  TurbVisc             4.8749e-14          0.1418      0.00048238       0.0064188
v  CourantNb              0.028622           42245          70.997          17.157
v  FourierNb               0.22198      2.3653e+06          217.38          2.7599
v  total_pressure       4.9887e+05      5.1471e+05      5.0967e+05      5.0795e+05
v  Local Time Step            0.01        0.071112        0.010003        0.010013


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6354      2.3886e+06          288.37          19.917


 TIME FOR THE TIME STEP              178:        0.14220E+03

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


 INSTANT    0.179000000E+02   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        -0.123322881E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640647E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11819E+01 0.14001E+01
   Friction velocity        uet   :  0.15399E-01 0.67825E+01
   Friction velocity        uk    :  0.15374E-01 0.67825E+01
   Dimensionless distance   yplus :  0.56724E-03 0.86191E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2457
   Nb of faces within the viscous sub-layer     :      28932
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42769E+00     332   0.15988E+00   0.89966E-01 0.18106E+01 
c  Velocity[X]                                      0.24547E-01 
c  Velocity[Y]                                      0.31182E-01 
c  Velocity[Z]                                      0.34237E-01 
c  Pressure     0.15072E-01     781   0.10590E-01   0.35244E-01 0.17688E-01 
c  k            0.15146E-01     131   0.20953E-03   0.70784E-05 0.17086E+01 
c  epsilon      0.86158E+02     156   0.25829E-03   0.15767E+03 0.48297E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00022605                            15
a  epsilon                 -0.3331                            21
a  Local Time Step      4.2278e-08                        281587


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9613          3.5244         0.35613         0.08113
v  Velocity[Y]             -3.5049          5.1194         0.25058         0.19179
v  Velocity[Z]             -5.9881          3.6135        -0.19607     -0.00037112
v  ǁVelocityǁ           0.00062702          6.6331          1.2226          1.5745
v  Pressure                -1131.9           14709          9667.7          7951.5
v  k                    6.9408e-09         0.35808       0.0042682       0.0079836
v  epsilon              6.1259e-05            5457            10.7          3.8643
v  TurbVisc              4.972e-14          0.1418      0.00048247       0.0064192
v  CourantNb             0.0031809           42737          71.012          17.156
v  FourierNb               0.22199      2.3653e+06          217.37          2.7597
v  total_pressure       4.9887e+05      5.1471e+05      5.0967e+05      5.0795e+05
v  Local Time Step            0.01         0.06808        0.010003        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6321      2.3897e+06          288.39          19.916


 TIME FOR THE TIME STEP              179:        0.14377E+03

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


 INSTANT    0.180000000E+02   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        -0.649724732E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640615E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11975E+01 0.14006E+01
   Friction velocity        uet   :  0.15391E-01 0.57231E+01
   Friction velocity        uk    :  0.15232E-01 0.57231E+01
   Dimensionless distance   yplus :  0.60574E-03 0.85954E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2460
   Nb of faces within the viscous sub-layer     :      28932
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42740E+00     322   0.15959E+00   0.92160E-01 0.18324E+01 
c  Velocity[X]                                      0.24503E-01 
c  Velocity[Y]                                      0.31590E-01 
c  Velocity[Z]                                      0.36067E-01 
c  Pressure     0.15022E-01     762   0.10622E-01   0.35133E-01 0.15372E-01 
c  k            0.15149E-01     136   0.18808E-03   0.76940E-05 0.17810E+01 
c  epsilon      0.86398E+02     126   0.21454E-03   0.19727E+03 0.53966E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021532                            19
a  epsilon                 -6.6561                            22
a  Local Time Step      4.2278e-08                        281593


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8515          3.5249         0.35605        0.081158
v  Velocity[Y]             -3.4829          5.1535         0.25061         0.19179
v  Velocity[Z]             -6.0745          3.5932        -0.19657     -0.00033716
v  ǁVelocityǁ           0.00050741          6.7227          1.2228          1.5746
v  Pressure                -1135.3           14711          9668.8          7952.3
v  k                    6.0404e-09         0.35752       0.0042644       0.0079845
v  epsilon              6.1301e-05          5442.6          10.658          3.8657
v  TurbVisc             4.9493e-14          0.1418      0.00048277       0.0064198
v  CourantNb             0.0064138           43555          70.924          17.156
v  FourierNb               0.22201      2.3653e+06          217.38          2.7601
v  total_pressure       4.9886e+05      5.1471e+05      5.0967e+05      5.0795e+05
v  Local Time Step            0.01        0.074888        0.010003        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6414      2.3879e+06           288.3          19.916


 TIME FOR THE TIME STEP              180:        0.13713E+03

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


 INSTANT    0.181000000E+02   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        -0.718252956E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640640E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11816E+01 0.13994E+01
   Friction velocity        uet   :  0.10399E-01 0.56153E+01
   Friction velocity        uk    :  0.10397E-01 0.56153E+01
   Dimensionless distance   yplus :  0.70418E-03 0.86300E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2457
   Nb of faces within the viscous sub-layer     :      28934
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42737E+00     312   0.15954E+00   0.96531E-01 0.18757E+01 
c  Velocity[X]                                      0.26930E-01 
c  Velocity[Y]                                      0.34288E-01 
c  Velocity[Z]                                      0.35313E-01 
c  Pressure     0.15508E-01     870   0.10907E-01   0.36254E-01 0.24865E-01 
c  k            0.15151E-01     136   0.20021E-03   0.64364E-05 0.16289E+01 
c  epsilon      0.86178E+02     138   0.24912E-03   0.16804E+03 0.49747E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00022662                            17
a  epsilon                -0.34617                            24
a  Local Time Step      4.2278e-08                        281589


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9128          3.5243         0.35601        0.081139
v  Velocity[Y]              -3.504          5.0921         0.25076         0.19183
v  Velocity[Z]              -5.992           3.616        -0.19688      -0.0003426
v  ǁVelocityǁ           0.00027708          6.6328           1.223          1.5745
v  Pressure                -1133.1           14714          9671.4          7954.2
v  k                    6.0781e-09           0.362       0.0042734       0.0079848
v  epsilon              6.1338e-05          5544.2          10.726          3.8662
v  TurbVisc             4.1235e-14          0.1418      0.00048275         0.00642
v  CourantNb             0.0032811           43896          70.979          17.158
v  FourierNb               0.22202      2.3653e+06          217.37          2.7605
v  total_pressure       4.9887e+05      5.1471e+05      5.0967e+05      5.0795e+05
v  Local Time Step            0.01        0.082377        0.010004        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6338      2.3893e+06          288.35          19.918


 TIME FOR THE TIME STEP              181:        0.14017E+03

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


 INSTANT    0.182000000E+02   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        -0.361755250E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640649E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11962E+01 0.13998E+01
   Friction velocity        uet   :  0.82693E-02 0.74881E+01
   Friction velocity        uk    :  0.82676E-02 0.74881E+01
   Dimensionless distance   yplus :  0.36818E-03 0.85966E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2452
   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     0.42716E+00     318   0.15409E+00   0.93261E-01 0.18434E+01 
c  Velocity[X]                                      0.26088E-01 
c  Velocity[Y]                                      0.32954E-01 
c  Velocity[Z]                                      0.34219E-01 
c  Pressure     0.15585E-01     794   0.10961E-01   0.36452E-01 0.17578E-01 
c  k            0.15151E-01     146   0.21229E-03   0.65549E-05 0.16434E+01 
c  epsilon      0.86370E+02     220   0.22951E-03   0.15311E+03 0.47549E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021998                            15
a  epsilon                 -6.5046                            21
a  Local Time Step      4.2278e-08                        281591


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8439          3.5417         0.35622        0.081098
v  Velocity[Y]             -3.4916          5.0981         0.25073         0.19185
v  Velocity[Z]             -6.0767          3.6127        -0.19645     -0.00036253
v  ǁVelocityǁ           0.00044019          6.7285           1.223          1.5746
v  Pressure                  -1136           14715          9672.6          7955.5
v  k                     6.302e-09         0.35524       0.0042688       0.0079876
v  epsilon              6.1283e-05            5392          10.668          3.8687
v  TurbVisc             4.4565e-14          0.1418      0.00048292       0.0064203
v  CourantNb              0.028253           43246          70.972          17.158
v  FourierNb               0.22203      2.3653e+06          217.37          2.7597
v  total_pressure       4.9886e+05      5.1472e+05      5.0967e+05      5.0796e+05
v  Local Time Step            0.01        0.090615        0.010004        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6268      2.3882e+06          288.35          19.918


 TIME FOR THE TIME STEP              182:        0.14077E+03

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


 INSTANT    0.183000000E+02   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        -0.175602187E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640652E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11804E+01 0.13978E+01
   Friction velocity        uet   :  0.10229E-01 0.63843E+01
   Friction velocity        uk    :  0.10228E-01 0.63843E+01
   Dimensionless distance   yplus :  0.75132E-03 0.87171E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2457
   Nb of faces within the viscous sub-layer     :      28926
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42756E+00     325   0.15483E+00   0.89244E-01 0.18031E+01 
c  Velocity[X]                                      0.24282E-01 
c  Velocity[Y]                                      0.30783E-01 
c  Velocity[Z]                                      0.34179E-01 
c  Pressure     0.15337E-01     910   0.10860E-01   0.35857E-01 0.39805E-01 
c  k            0.15149E-01     137   0.20461E-03   0.80179E-05 0.18178E+01 
c  epsilon      0.86151E+02     144   0.23972E-03   0.18049E+03 0.51554E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.000155                            19
a  epsilon                -0.33833                            28
a  Local Time Step      4.2278e-08                        281582


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -1.962          3.5068         0.35611        0.081027
v  Velocity[Y]             -3.5089          5.0805         0.24989         0.19182
v  Velocity[Z]             -5.9808          3.5852        -0.19609     -0.00039516
v  ǁVelocityǁ           0.00030993          6.6253          1.2225          1.5748
v  Pressure                -1135.1           14711          9668.6          7952.1
v  k                    6.3252e-09          0.3623        0.004271       0.0079884
v  epsilon              6.1046e-05          5552.2          10.721          3.8692
v  TurbVisc             4.5293e-14          0.1418      0.00048308       0.0064204
v  CourantNb              0.035524           43093          70.969          17.158
v  FourierNb               0.22205      2.3653e+06          217.37          2.7605
v  total_pressure       4.9886e+05      5.1471e+05      5.0967e+05      5.0795e+05
v  Local Time Step            0.01        0.099676        0.010004        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6352      2.3902e+06          288.34          19.919


 TIME FOR THE TIME STEP              183:        0.14182E+03

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


 INSTANT    0.184000000E+02   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        -0.646135009E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699641016E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11958E+01 0.14020E+01
   Friction velocity        uet   :  0.11980E-01 0.53157E+01
   Friction velocity        uk    :  0.11976E-01 0.53157E+01
   Dimensionless distance   yplus :  0.46943E-03 0.87343E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2456
   Nb of faces within the viscous sub-layer     :      28927
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42733E+00     307   0.15541E+00   0.90321E-01 0.18139E+01 
c  Velocity[X]                                      0.24820E-01 
c  Velocity[Y]                                      0.31864E-01 
c  Velocity[Z]                                      0.33636E-01 
c  Pressure     0.15412E-01     613   0.10777E-01   0.36030E-01 0.10361E-01 
c  k            0.15153E-01     131   0.19065E-03   0.63377E-05 0.16161E+01 
c  epsilon      0.86438E+02     158   0.23911E-03   0.16856E+03 0.49957E+01 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00022557                            17
a  epsilon                 -6.5216                            26
a  Local Time Step      4.2278e-08                        281599


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9281          3.5243         0.35623        0.080992
v  Velocity[Y]              -3.481          5.0145         0.24973         0.19183
v  Velocity[Z]              -6.052          3.6163         -0.1963     -0.00043032
v  ǁVelocityǁ           0.00081437          6.7006          1.2228          1.5747
v  Pressure                -1134.6           14711          9668.3          7951.9
v  k                    6.4671e-09         0.35765       0.0042595       0.0079884
v  epsilon              6.0802e-05          5440.8          10.628          3.8652
v  TurbVisc             4.5593e-14          0.1418      0.00048261       0.0064206
v  CourantNb               0.02126           43234          70.919          17.157
v  FourierNb               0.22205      2.3653e+06          217.37          2.7603
v  total_pressure       4.9887e+05      5.1471e+05      5.0967e+05      5.0795e+05
v  Local Time Step            0.01         0.10964        0.010004        0.010012


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6317      2.3885e+06          288.29          19.918


 TIME FOR THE TIME STEP              184:        0.12471E+03

===============================================================


 INSTANT    0.185000000E+02   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        -0.179893608E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699641000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11806E+01 0.14007E+01
   Friction velocity        uet   :  0.13913E-01 0.50491E+01
   Friction velocity        uk    :  0.13909E-01 0.50491E+01
   Dimensionless distance   yplus :  0.63834E-03 0.86102E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2466
   Nb of faces within the viscous sub-layer     :      28921
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42750E+00     339   0.15499E+00   0.88471E-01 0.17952E+01 
c  Velocity[X]                                      0.24576E-01 
c  Velocity[Y]                                      0.30811E-01 
c  Velocity[Z]                                      0.33083E-01 
c  Pressure     0.14900E-01     684   0.10456E-01   0.34813E-01 0.10804E-01 
c  k            0.15147E-01     136   0.20913E-03   0.67923E-05 0.16730E+01 
c  epsilon      0.86109E+02     148   0.26348E-03   0.19390E+03 0.53537E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00020327                            15
a  epsilon                -0.33368                            22
a  Local Time Step      4.2278e-08                        281593


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9838          3.5228         0.35644         0.08097
v  Velocity[Y]             -3.5119          5.0184         0.25017         0.19182
v  Velocity[Z]             -5.9898           3.609        -0.19632     -0.00043292
v  ǁVelocityǁ           0.00074271          6.6347           1.223          1.5747
v  Pressure                -1133.4           14712            9669          7952.3
v  k                    7.7552e-09         0.35573       0.0042748       0.0079898
v  epsilon              6.0599e-05          5388.9          10.718          3.8689
v  TurbVisc             4.6126e-14          0.1418      0.00048267       0.0064209
v  CourantNb            0.00054956           42443          70.968          17.159
v  FourierNb               0.22206      2.3653e+06          217.37            2.76
v  total_pressure       4.9887e+05      5.1471e+05      5.0967e+05      5.0795e+05
v  Local Time Step            0.01        0.077532        0.010003        0.010011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6327      2.3911e+06          288.34          19.919


 TIME FOR THE TIME STEP              185:        0.13423E+03

===============================================================


 INSTANT    0.186000000E+02   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        -0.194244622E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640662E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11972E+01 0.13988E+01
   Friction velocity        uet   :  0.16844E-01 0.68114E+01
   Friction velocity        uk    :  0.16637E-01 0.68114E+01
   Dimensionless distance   yplus :  0.63997E-03 0.88153E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2461
   Nb of faces within the viscous sub-layer     :      28920
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42754E+00     327   0.15970E+00   0.89262E-01 0.18032E+01 
c  Velocity[X]                                      0.24110E-01 
c  Velocity[Y]                                      0.31247E-01 
c  Velocity[Z]                                      0.33905E-01 
c  Pressure     0.14872E-01     647   0.10467E-01   0.34741E-01 0.13709E-01 
c  k            0.15153E-01     150   0.18603E-03   0.63390E-05 0.16161E+01 
c  epsilon      0.86248E+02     234   0.22467E-03   0.15383E+03 0.47695E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021016                            17
a  epsilon                 -6.5169                            21
a  Local Time Step      4.2278e-08                        281601


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8612          3.5192         0.35663        0.080989
v  Velocity[Y]             -3.4949          5.0773         0.25006         0.19185
v  Velocity[Z]             -6.0461          3.5913        -0.19658     -0.00041224
v  ǁVelocityǁ           0.00065586          6.6915          1.2232          1.5748
v  Pressure                -1137.1           14712          9669.5          7952.3
v  k                    6.1881e-09         0.35595       0.0042688       0.0079913
v  epsilon              6.0296e-05          5391.7          10.659          3.8692
v  TurbVisc             5.3025e-14          0.1418      0.00048331       0.0064213
v  CourantNb              0.030852           43028          70.975          17.159
v  FourierNb               0.22207      2.3653e+06          217.38          2.7604
v  total_pressure       4.9886e+05      5.1471e+05      5.0967e+05      5.0795e+05
v  Local Time Step            0.01        0.075392        0.010003        0.010011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6329      2.3891e+06          288.35          19.919


 TIME FOR THE TIME STEP              186:        0.13228E+03

===============================================================


 INSTANT    0.187000000E+02   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        -0.778044215E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640669E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11833E+01 0.13981E+01
   Friction velocity        uet   :  0.15259E-01 0.76442E+01
   Friction velocity        uk    :  0.15202E-01 0.76442E+01
   Dimensionless distance   yplus :  0.97541E-03 0.86641E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2460
   Nb of faces within the viscous sub-layer     :      28932
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42693E+00     318   0.15652E+00   0.91121E-01 0.18220E+01 
c  Velocity[X]                                      0.24951E-01 
c  Velocity[Y]                                      0.32974E-01 
c  Velocity[Z]                                      0.33197E-01 
c  Pressure     0.15484E-01     649   0.10724E-01   0.36183E-01 0.11164E-01 
c  k            0.15154E-01     134   0.21125E-03   0.69732E-05 0.16951E+01 
c  epsilon      0.86150E+02     147   0.26936E-03   0.16754E+03 0.49680E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00020807                            21
a  epsilon                -0.34305                            29
a  Local Time Step      4.2278e-08                        281588


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9949          3.5221         0.35654        0.081042
v  Velocity[Y]             -3.5081          5.0449         0.24998         0.19185
v  Velocity[Z]             -5.9616          3.6136        -0.19673     -0.00036337
v  ǁVelocityǁ           0.00066813          6.6115          1.2232          1.5747
v  Pressure                  -1136           14713          9669.9          7952.8
v  k                    6.0107e-09         0.35979       0.0042689       0.0079904
v  epsilon              6.0047e-05          5481.2          10.712          3.8695
v  TurbVisc             4.3895e-14          0.1418      0.00048287       0.0064213
v  CourantNb             0.0029817           41865          70.946          17.161
v  FourierNb               0.22207      2.3653e+06          217.37          2.7598
v  total_pressure       4.9886e+05      5.1471e+05      5.0967e+05      5.0795e+05
v  Local Time Step            0.01        0.079568        0.010004        0.010011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6366      2.3875e+06          288.32          19.921


 TIME FOR THE TIME STEP              187:        0.12905E+03

===============================================================


 INSTANT    0.188000000E+02   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        -0.103885361E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640639E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11978E+01 0.13999E+01
   Friction velocity        uet   :  0.93654E-02 0.49885E+01
   Friction velocity        uk    :  0.93512E-02 0.49885E+01
   Dimensionless distance   yplus :  0.53956E-03 0.88226E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2457
   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     0.42723E+00     323   0.15587E+00   0.88693E-01 0.17976E+01 
c  Velocity[X]                                      0.25117E-01 
c  Velocity[Y]                                      0.31219E-01 
c  Velocity[Z]                                      0.32357E-01 
c  Pressure     0.14752E-01     834   0.10288E-01   0.34497E-01 0.24600E-01 
c  k            0.15154E-01     139   0.19505E-03   0.65819E-05 0.16469E+01 
c  epsilon      0.86300E+02     160   0.23894E-03   0.15398E+03 0.47743E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00020676                            16
a  epsilon                  -6.704                            24
a  Local Time Step      4.2278e-08                        281601


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9274          3.5268         0.35653        0.081075
v  Velocity[Y]             -3.4879          5.0927          0.2502         0.19183
v  Velocity[Z]              -6.037          3.6122        -0.19675     -0.00037243
v  ǁVelocityǁ           0.00069945           6.687          1.2231          1.5746
v  Pressure                -1140.2           14710          9667.8          7951.3
v  k                    7.6537e-09         0.35555       0.0042638       0.0079905
v  epsilon              5.9948e-05          5382.2          10.652          3.8669
v  TurbVisc             4.1931e-14          0.1418       0.0004826       0.0064214
v  CourantNb              0.011964           42497           70.97          17.159
v  FourierNb               0.22207      2.3653e+06          217.37          2.7601
v  total_pressure       4.9886e+05      5.1471e+05      5.0967e+05      5.0795e+05
v  Local Time Step            0.01        0.087525        0.010003        0.010011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6339      2.3871e+06          288.34          19.919


 TIME FOR THE TIME STEP              188:        0.13822E+03

===============================================================


 INSTANT    0.189000000E+02   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        -0.307035528E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699641004E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11857E+01 0.13853E+01
   Friction velocity        uet   :  0.14746E-01 0.81745E+01
   Friction velocity        uk    :  0.14742E-01 0.81745E+01
   Dimensionless distance   yplus :  0.10431E-02 0.86353E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2466
   Nb of faces within the viscous sub-layer     :      28922
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42752E+00     326   0.15703E+00   0.85999E-01 0.17699E+01 
c  Velocity[X]                                      0.23199E-01 
c  Velocity[Y]                                      0.30473E-01 
c  Velocity[Z]                                      0.32327E-01 
c  Pressure     0.14473E-01     671   0.10094E-01   0.33836E-01 0.12002E-01 
c  k            0.15144E-01     137   0.19746E-03   0.55813E-05 0.15166E+01 
c  epsilon      0.85183E+02     134   0.24787E-03   0.16457E+03 0.49401E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00020387                            15
a  epsilon                -0.33704                            21
a  Local Time Step      4.2278e-08                        281594


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9221          3.5288         0.35637        0.081057
v  Velocity[Y]             -3.5114          5.1015         0.25024         0.19182
v  Velocity[Z]             -6.0189          3.5776        -0.19705      -0.0004063
v  ǁVelocityǁ           0.00035458          6.6675          1.2232          1.5748
v  Pressure                -1142.6           14710          9668.3          7951.9
v  k                    5.9874e-09         0.35891       0.0042708       0.0079919
v  epsilon              5.9859e-05          5467.3            10.7          3.8683
v  TurbVisc             5.3146e-14          0.1418       0.0004828       0.0064215
v  CourantNb              0.013344           41463          70.929          17.159
v  FourierNb               0.22207      2.3653e+06          217.37          2.7599
v  total_pressure       4.9886e+05      5.1471e+05      5.0967e+05      5.0795e+05
v  Local Time Step            0.01        0.082585        0.010003        0.010011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6343      2.3876e+06           288.3          19.919


 TIME FOR THE TIME STEP              189:        0.13034E+03

===============================================================


 INSTANT    0.190000000E+02   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        -0.779254112E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640647E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12036E+01 0.13966E+01
   Friction velocity        uet   :  0.38773E-02 0.56606E+01
   Friction velocity        uk    :  0.40016E-02 0.56606E+01
   Dimensionless distance   yplus :  0.72229E-03 0.87806E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2461
   Nb of faces within the viscous sub-layer     :      28927
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42702E+00     323   0.15602E+00   0.88854E-01 0.17992E+01 
c  Velocity[X]                                      0.23537E-01 
c  Velocity[Y]                                      0.32060E-01 
c  Velocity[Z]                                      0.33257E-01 
c  Pressure     0.15009E-01     689   0.10456E-01   0.35073E-01 0.11336E-01 
c  k            0.15153E-01     148   0.19311E-03   0.64420E-05 0.16291E+01 
c  epsilon      0.86248E+02     232   0.24603E-03   0.19997E+03 0.54337E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0002106                            17
a  epsilon                  -6.342                            25
a  Local Time Step      4.2278e-08                        281595


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9062          3.5272         0.35631        0.081062
v  Velocity[Y]             -3.4853          5.1563         0.25053         0.19185
v  Velocity[Z]             -6.0042          3.6078        -0.19691     -0.00040787
v  ǁVelocityǁ           0.00023757          6.6482          1.2233          1.5747
v  Pressure                -1147.5           14711          9668.9          7952.3
v  k                    5.8498e-09         0.35801       0.0042642       0.0079916
v  epsilon              5.9681e-05          5450.2          10.657          3.8682
v  TurbVisc             4.1298e-14          0.1418      0.00048282       0.0064218
v  CourantNb                0.0335           41286           70.97          17.161
v  FourierNb               0.22207      2.3653e+06          217.37            2.76
v  total_pressure       4.9885e+05      5.1471e+05      5.0967e+05      5.0795e+05
v  Local Time Step            0.01        0.090843        0.010003        0.010011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6331      2.3885e+06          288.34          19.921


 TIME FOR THE TIME STEP              190:        0.13432E+03

===============================================================


 INSTANT    0.191000000E+02   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        -0.396654318E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640647E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11834E+01 0.13868E+01
   Friction velocity        uet   :  0.11300E-01 0.76423E+01
   Friction velocity        uk    :  0.11297E-01 0.76423E+01
   Dimensionless distance   yplus :  0.97516E-03 0.86217E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2456
   Nb of faces within the viscous sub-layer     :      28925
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42712E+00     320   0.15736E+00   0.88915E-01 0.17997E+01 
c  Velocity[X]                                      0.24163E-01 
c  Velocity[Y]                                      0.31476E-01 
c  Velocity[Z]                                      0.33276E-01 
c  Pressure     0.14805E-01     811   0.10294E-01   0.34594E-01 0.18029E-01 
c  k            0.15143E-01     135   0.17595E-03   0.50440E-05 0.14418E+01 
c  epsilon      0.85091E+02     135   0.24178E-03   0.11928E+03 0.42039E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021398                            19
a  epsilon                -0.33843                            28
a  Local Time Step      4.2278e-08                        281587


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9987          3.5357         0.35605        0.081089
v  Velocity[Y]             -3.5057          5.1073         0.25064         0.19186
v  Velocity[Z]             -6.0316          3.6077        -0.19695     -0.00042038
v  ǁVelocityǁ           0.00033697          6.6783          1.2233          1.5748
v  Pressure                -1147.1           14713          9670.5          7953.6
v  k                    6.3863e-09         0.35858       0.0042679       0.0079912
v  epsilon              2.1905e-05          5465.1          10.695          3.8668
v  TurbVisc             4.2509e-14          0.1418      0.00048254       0.0064217
v  CourantNb              0.007441           40579          70.987          17.161
v  FourierNb               0.22208      2.3653e+06          217.37          2.7597
v  total_pressure       4.9885e+05      5.1471e+05      5.0967e+05      5.0795e+05
v  Local Time Step            0.01        0.082927        0.010003        0.010011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6275      2.3889e+06          288.36           19.92


 TIME FOR THE TIME STEP              191:        0.13632E+03

===============================================================


 INSTANT    0.192000000E+02   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        -0.668791125E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640638E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11994E+01 0.13954E+01
   Friction velocity        uet   :  0.12292E-01 0.55459E+01
   Friction velocity        uk    :  0.12289E-01 0.55459E+01
   Dimensionless distance   yplus :  0.66178E-03 0.87802E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2464
   Nb of faces within the viscous sub-layer     :      28928
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42713E+00     312   0.16251E+00   0.88882E-01 0.17995E+01 
c  Velocity[X]                                      0.24146E-01 
c  Velocity[Y]                                      0.29686E-01 
c  Velocity[Z]                                      0.35050E-01 
c  Pressure     0.14835E-01     809   0.10354E-01   0.34667E-01 0.17361E-01 
c  k            0.15149E-01     140   0.17808E-03   0.58704E-05 0.15552E+01 
c  epsilon      0.86154E+02     159   0.23077E-03   0.14687E+03 0.46602E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00020233                            16
a  epsilon                 -6.5506                            23
a  Local Time Step      4.2278e-08                        281593


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9284          3.5238         0.35603        0.081064
v  Velocity[Y]             -3.4825          5.1295         0.25075         0.19185
v  Velocity[Z]              -5.985          3.5948        -0.19692     -0.00038082
v  ǁVelocityǁ           0.00061515          6.6306          1.2233          1.5747
v  Pressure                -1152.5           14710          9668.9          7952.5
v  k                    7.7813e-09          0.3601       0.0042673       0.0079921
v  epsilon              5.9558e-05          5499.9          10.663          3.8683
v  TurbVisc             4.6989e-14          0.1418      0.00048285       0.0064218
v  CourantNb             0.0080094           41105          70.968          17.161
v  FourierNb               0.22208      2.3653e+06          217.37          2.7598
v  total_pressure       4.9885e+05      5.1471e+05      5.0967e+05      5.0795e+05
v  Local Time Step            0.01        0.070562        0.010003         0.01001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6375      2.3874e+06          288.34          19.921


 TIME FOR THE TIME STEP              192:        0.13719E+03

===============================================================


 INSTANT    0.193000000E+02   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        -0.642421530E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699641009E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11834E+01 0.13856E+01
   Friction velocity        uet   :  0.13175E-01 0.81790E+01
   Friction velocity        uk    :  0.13171E-01 0.81790E+01
   Dimensionless distance   yplus :  0.10436E-02 0.86221E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2464
   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     0.42736E+00     327   0.15942E+00   0.96694E-01 0.18770E+01 
c  Velocity[X]                                      0.26224E-01 
c  Velocity[Y]                                      0.34423E-01 
c  Velocity[Z]                                      0.36047E-01 
c  Pressure     0.15635E-01     752   0.10894E-01   0.36559E-01 0.15668E-01 
c  k            0.15149E-01     151   0.18725E-03   0.65129E-05 0.16382E+01 
c  epsilon      0.85128E+02     218   0.24266E-03   0.16878E+03 0.49940E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021054                            17
a  epsilon                -0.32833                            25
a  Local Time Step      4.2278e-08                        281586


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.0063          3.5123         0.35619        0.081083
v  Velocity[Y]             -3.4993          5.1805         0.25076         0.19186
v  Velocity[Z]             -6.0265           3.614        -0.19695     -0.00041212
v  ǁVelocityǁ           0.00039886          6.6691          1.2236          1.5747
v  Pressure                -1154.7           14708          9667.9          7951.6
v  k                     5.387e-09         0.35866       0.0042693       0.0079923
v  epsilon              5.9527e-05          5467.6          10.685          3.8697
v  TurbVisc             5.3297e-14          0.1418      0.00048266       0.0064218
v  CourantNb              0.025719           41277          70.978          17.161
v  FourierNb               0.22209      2.3653e+06          217.37          2.7601
v  total_pressure       4.9885e+05      5.1471e+05      5.0967e+05      5.0795e+05
v  Local Time Step            0.01        0.071962        0.010003        0.010011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6441      2.3901e+06          288.35          19.921


 TIME FOR THE TIME STEP              193:        0.13802E+03

===============================================================


 INSTANT    0.194000000E+02   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        -0.762293269E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640983E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11970E+01 0.13945E+01
   Friction velocity        uet   :  0.73758E-02 0.68464E+01
   Friction velocity        uk    :  0.73749E-02 0.68464E+01
   Dimensionless distance   yplus :  0.87361E-03 0.87531E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2465
   Nb of faces within the viscous sub-layer     :      28931
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42697E+00     323   0.15449E+00   0.93936E-01 0.18500E+01 
c  Velocity[X]                                      0.25054E-01 
c  Velocity[Y]                                      0.32440E-01 
c  Velocity[Z]                                      0.36442E-01 
c  Pressure     0.14813E-01     870   0.10307E-01   0.34643E-01 0.25785E-01 
c  k            0.15157E-01     143   0.19843E-03   0.69922E-05 0.16972E+01 
c  epsilon      0.86156E+02     128   0.33451E-03   0.30720E+03 0.67280E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0002064                            21
a  epsilon                 -6.6137                            25
a  Local Time Step      4.2278e-08                        281603


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8732          3.5295         0.35689        0.081101
v  Velocity[Y]             -3.4775          5.1594         0.25071          0.1918
v  Velocity[Z]             -6.0354          3.6066        -0.19607     -0.00042439
v  ǁVelocityǁ           0.00064995          6.6836          1.2236          1.5746
v  Pressure                  -1161           14705          9664.7          7949.5
v  k                    5.8036e-09          0.3578       0.0042655       0.0079914
v  epsilon              5.9509e-05          5446.7          10.729          3.8697
v  TurbVisc             3.7684e-14          0.1418      0.00048208       0.0064218
v  CourantNb              0.018608           42541           71.01           17.16
v  FourierNb                0.2221      2.3653e+06          217.37          2.7599
v  total_pressure       4.9884e+05       5.147e+05      5.0966e+05      5.0795e+05
v  Local Time Step            0.01        0.079158        0.010003        0.010011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6423      2.3876e+06          288.38           19.92


 TIME FOR THE TIME STEP              194:        0.14111E+03

===============================================================


 INSTANT    0.195000000E+02   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        -0.777839097E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699641001E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11814E+01 0.13887E+01
   Friction velocity        uet   :  0.17379E-01 0.60445E+01
   Friction velocity        uk    :  0.17374E-01 0.60445E+01
   Dimensionless distance   yplus :  0.76586E-03 0.85911E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2462
   Nb of faces within the viscous sub-layer     :      28927
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42718E+00     321   0.15414E+00   0.87229E-01 0.17826E+01 
c  Velocity[X]                                      0.22431E-01 
c  Velocity[Y]                                      0.31726E-01 
c  Velocity[Z]                                      0.33073E-01 
c  Pressure     0.14568E-01     726   0.10149E-01   0.34041E-01 0.11377E-01 
c  k            0.15139E-01     139   0.18913E-03   0.60417E-05 0.15781E+01 
c  epsilon      0.85027E+02     152   0.31199E-03   0.23533E+03 0.59080E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00020106                            14
a  epsilon                -0.32473                            22
a  Local Time Step      4.2278e-08                        281587


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]               -1.99          3.5178         0.35666         0.08113
v  Velocity[Y]             -3.5019          5.1678         0.25045         0.19181
v  Velocity[Z]             -5.9922          3.5866        -0.19582     -0.00044604
v  ǁVelocityǁ           0.00060619          6.6342          1.2232          1.5748
v  Pressure                -1163.3           14704          9663.7          7948.9
v  k                    6.3584e-09         0.36188        0.004259       0.0079901
v  epsilon              5.9505e-05          5539.3          10.659          3.8654
v  TurbVisc             4.2038e-14          0.1418       0.0004818       0.0064215
v  CourantNb              0.018549           43723          71.038          17.159
v  FourierNb                0.2221      2.3653e+06          217.37          2.7598
v  total_pressure       4.9884e+05       5.147e+05      5.0966e+05      5.0795e+05
v  Local Time Step            0.01        0.082745        0.010003        0.010011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6473      2.3876e+06          288.41          19.919


 TIME FOR THE TIME STEP              195:        0.13354E+03

===============================================================


 INSTANT    0.196000000E+02   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        -0.499571364E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699641012E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11960E+01 0.13951E+01
   Friction velocity        uet   :  0.15331E-01 0.64865E+01
   Friction velocity        uk    :  0.15173E-01 0.64865E+01
   Dimensionless distance   yplus :  0.72415E-03 0.87375E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2459
   Nb of faces within the viscous sub-layer     :      28925
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42714E+00     325   0.15554E+00   0.88571E-01 0.17965E+01 
c  Velocity[X]                                      0.22711E-01 
c  Velocity[Y]                                      0.32449E-01 
c  Velocity[Z]                                      0.33412E-01 
c  Pressure     0.14679E-01     901   0.10267E-01   0.34302E-01 0.29873E-01 
c  k            0.15152E-01     150   0.18753E-03   0.62957E-05 0.16106E+01 
c  epsilon      0.86087E+02     232   0.22683E-03   0.11898E+03 0.41943E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00020067                            17
a  epsilon                 -6.4969                            27
a  Local Time Step      4.2278e-08                        281599


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9328          3.5241         0.35639        0.081139
v  Velocity[Y]             -3.4743          5.2389         0.25049         0.19186
v  Velocity[Z]             -6.0497          3.6181        -0.19616      -0.0003968
v  ǁVelocityǁ           0.00075134           6.697          1.2232          1.5746
v  Pressure                -1165.4           14700          9660.2          7946.4
v  k                    6.4039e-09          0.3562       0.0042596       0.0079899
v  epsilon              5.9449e-05          5405.7          10.659          3.8664
v  TurbVisc              4.651e-14          0.1418       0.0004816       0.0064214
v  CourantNb             0.0097119           43934           70.99           17.16
v  FourierNb                0.2221      2.3653e+06          217.37          2.7605
v  total_pressure       4.9883e+05       5.147e+05      5.0966e+05      5.0795e+05
v  Local Time Step            0.01         0.08412        0.010003        0.010012


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6422      2.3883e+06          288.36          19.921


 TIME FOR THE TIME STEP              196:        0.14730E+03

===============================================================


 INSTANT    0.197000000E+02   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         0.209862487E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640993E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11809E+01 0.13846E+01
   Friction velocity        uet   :  0.14112E-01 0.47701E+01
   Friction velocity        uk    :  0.14109E-01 0.47701E+01
   Dimensionless distance   yplus :  0.60132E-03 0.86168E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2455
   Nb of faces within the viscous sub-layer     :      28927
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42737E+00     317   0.15747E+00   0.92619E-01 0.18369E+01 
c  Velocity[X]                                      0.25920E-01 
c  Velocity[Y]                                      0.31830E-01 
c  Velocity[Z]                                      0.34869E-01 
c  Pressure     0.14624E-01     795   0.10225E-01   0.34181E-01 0.18110E-01 
c  k            0.15138E-01     142   0.19588E-03   0.62622E-05 0.16067E+01 
c  epsilon      0.84992E+02     131   0.23097E-03   0.13899E+03 0.45416E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00020107                            20
a  epsilon                -0.33016                            26
a  Local Time Step      4.2278e-08                        281595


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9315          3.5201         0.35633        0.081096
v  Velocity[Y]             -3.5047          5.1775         0.25048         0.19189
v  Velocity[Z]             -5.9632          3.6092        -0.19628     -0.00036618
v  ǁVelocityǁ           0.00040536          6.6068          1.2233          1.5747
v  Pressure                -1163.6           14703          9661.6          7947.8
v  k                    6.5174e-09          0.3606       0.0042631       0.0079888
v  epsilon               5.933e-05          5504.2          10.661          3.8641
v  TurbVisc             4.6204e-14          0.1418       0.0004815       0.0064212
v  CourantNb            0.00067048           41837          70.995          17.159
v  FourierNb               0.22209      2.3653e+06          217.37          2.7601
v  total_pressure       4.9884e+05       5.147e+05      5.0966e+05      5.0795e+05
v  Local Time Step            0.01        0.072938        0.010003        0.010011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6411      2.3892e+06          288.37          19.919


 TIME FOR THE TIME STEP              197:        0.13424E+03

===============================================================


 INSTANT    0.198000000E+02   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        -0.938015569E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640654E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11965E+01 0.13951E+01
   Friction velocity        uet   :  0.11336E-01 0.56193E+01
   Friction velocity        uk    :  0.11335E-01 0.56193E+01
   Dimensionless distance   yplus :  0.71702E-03 0.87383E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2459
   Nb of faces within the viscous sub-layer     :      28921
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42712E+00     329   0.16169E+00   0.95253E-01 0.18629E+01 
c  Velocity[X]                                      0.24237E-01 
c  Velocity[Y]                                      0.34827E-01 
c  Velocity[Z]                                      0.36189E-01 
c  Pressure     0.14810E-01     777   0.10335E-01   0.34592E-01 0.15701E-01 
c  k            0.15153E-01     137   0.20871E-03   0.62863E-05 0.16093E+01 
c  epsilon      0.86219E+02     155   0.24543E-03   0.19145E+03 0.53134E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00019639                            17
a  epsilon                 -6.5206                            22
a  Local Time Step      4.2278e-08                        281593


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9551          3.5269         0.35633        0.081072
v  Velocity[Y]             -3.4845           5.257         0.25031         0.19191
v  Velocity[Z]              -6.066          3.5871        -0.19634     -0.00037256
v  ǁVelocityǁ           0.00042653           6.714          1.2233          1.5747
v  Pressure                -1164.5           14704          9663.3          7948.8
v  k                     6.406e-09         0.35377       0.0042644       0.0079902
v  epsilon              5.9123e-05          5355.8          10.699          3.8687
v  TurbVisc             4.6506e-14          0.1418      0.00048159       0.0064212
v  CourantNb              0.027874           42177          70.964           17.16
v  FourierNb               0.22209      2.3653e+06          217.37          2.7605
v  total_pressure       4.9884e+05       5.147e+05      5.0966e+05      5.0795e+05
v  Local Time Step            0.01        0.080231        0.010004        0.010012


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6561      2.3865e+06          288.34          19.921


 TIME FOR THE TIME STEP              198:        0.13833E+03

===============================================================


 INSTANT    0.199000000E+02   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        -0.535956371E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640640E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11852E+01 0.13889E+01
   Friction velocity        uet   :  0.68080E-02 0.47135E+01
   Friction velocity        uk    :  0.68276E-02 0.47135E+01
   Dimensionless distance   yplus :  0.52472E-03 0.85834E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2461
   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     0.42712E+00     331   0.15802E+00   0.94638E-01 0.18569E+01 
c  Velocity[X]                                      0.25242E-01 
c  Velocity[Y]                                      0.33926E-01 
c  Velocity[Z]                                      0.35470E-01 
c  Pressure     0.15119E-01     866   0.10524E-01   0.35328E-01 0.27782E-01 
c  k            0.15144E-01     146   0.20066E-03   0.71515E-05 0.17167E+01 
c  epsilon      0.84989E+02     134   0.25142E-03   0.17848E+03 0.51379E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0002008                            18
a  epsilon                -0.32623                            23
a  Local Time Step      4.2278e-08                        281581


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9994          3.5219         0.35649        0.081097
v  Velocity[Y]             -3.5028          5.2192          0.2504         0.19193
v  Velocity[Z]             -5.9682          3.6144        -0.19656     -0.00037469
v  ǁVelocityǁ           0.00034567          6.6075          1.2234          1.5747
v  Pressure                -1161.8           14708          9666.3          7950.9
v  k                    6.4345e-09         0.36127       0.0042631       0.0079908
v  epsilon              5.8982e-05            5522          10.677          3.8672
v  TurbVisc             4.6017e-14          0.1418      0.00048139        0.006421
v  CourantNb             0.0068383           41311          71.008          17.161
v  FourierNb               0.22207      2.3653e+06          217.37          2.7603
v  total_pressure       4.9884e+05      5.1471e+05      5.0967e+05      5.0795e+05
v  Local Time Step            0.01        0.088255        0.010004        0.010012


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6593      2.3897e+06          288.38          19.921


 TIME FOR THE TIME STEP              199:        0.14028E+03

===============================================================


 INSTANT    0.200000000E+02   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        -0.934835988E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640661E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11959E+01 0.13943E+01
   Friction velocity        uet   :  0.44717E-02 0.43385E+01
   Friction velocity        uk    :  0.44712E-02 0.43385E+01
   Dimensionless distance   yplus :  0.42248E-03 0.87328E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2457
   Nb of faces within the viscous sub-layer     :      28924
   Total number of wall faces                   :      41000
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration        200, Physical time    0.20000E+02


   ** 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 the external forces                      
 End writing


 Time for restart files:    0.11093E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42719E+00     323   0.15537E+00   0.93884E-01 0.18495E+01 
c  Velocity[X]                                      0.24100E-01 
c  Velocity[Y]                                      0.33050E-01 
c  Velocity[Z]                                      0.36734E-01 
c  Pressure     0.14609E-01     799   0.10157E-01   0.34169E-01 0.20155E-01 
c  k            0.15153E-01     134   0.19278E-03   0.67359E-05 0.16658E+01 
c  epsilon      0.86139E+02     148   0.23758E-03   0.15504E+03 0.47848E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00019832                            15
a  epsilon                 -6.6122                            23
a  Local Time Step      4.2278e-08                        281595


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9327          3.5357         0.35642         0.08111
v  Velocity[Y]             -3.4847          5.2119         0.25062         0.19194
v  Velocity[Z]             -6.0495          3.6037        -0.19654     -0.00038676
v  ǁVelocityǁ           0.00072997          6.7047          1.2234          1.5746
v  Pressure                -1158.6           14710          9668.4          7952.4
v  k                    6.4448e-09         0.35576       0.0042589       0.0079908
v  epsilon              1.2253e-05            5397          10.672          3.8674
v  TurbVisc             4.5474e-14          0.1418      0.00048125       0.0064213
v  CourantNb              0.025922           40541          70.975          17.161
v  FourierNb               0.22206      2.3653e+06          217.37          2.7602
v  total_pressure       4.9884e+05      5.1471e+05      5.0967e+05      5.0795e+05
v  Local Time Step            0.01         0.09708        0.010004        0.010012


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6612      2.3858e+06          288.35          19.922


 TIME FOR THE TIME STEP              200:        0.14084E+03

===============================================================


 INSTANT    0.201000000E+02   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        -0.121953819E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640651E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11838E+01 0.13844E+01
   Friction velocity        uet   :  0.16526E-01 0.65865E+01
   Friction velocity        uk    :  0.16352E-01 0.65865E+01
   Dimensionless distance   yplus :  0.65024E-03 0.85766E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2461
   Nb of faces within the viscous sub-layer     :      28924
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47094E+00     325   0.14419E+00   0.20652E+02 0.21920E+02 
c  Velocity[X]                                      0.80737E+00 
c  Velocity[Y]                                      0.16499E+01 
c  Velocity[Z]                                      0.18195E+02 
c  Pressure     0.19917E-01    1916   0.31507E+00   0.46527E-01 0.50847E+02 
c  k            0.22020E-01     175   0.10705E-02   0.21218E-02 0.23604E+02 
c  epsilon      0.85143E+02     187   0.44795E-03   0.56268E+03 0.93293E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001677                            12
a  epsilon                -0.36478                            18
a  Local Time Step      4.2278e-08                        281587


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9241          5.1932         0.43734          0.1068
v  Velocity[Y]             -4.1562          6.8333         0.34941         0.24783
v  Velocity[Z]             -7.8565          4.4812        -0.21569       0.0065567
v  ǁVelocityǁ            0.0011424          9.3303          1.4165           1.977
v  Pressure                -2.3159           31740           18962           17064
v  k                     6.717e-09         0.34692        0.004556       0.0094429
v  epsilon              6.1153e-05          5321.9          11.317          4.0463
v  TurbVisc              4.583e-14          0.1418      0.00048122       0.0064213
v  CourantNb             0.0042103           39210          70.961           17.16
v  FourierNb               0.22206      2.3653e+06          217.37          2.7605
v  total_pressure            5e+05      5.3174e+05      5.1896e+05      5.1706e+05
v  Local Time Step            0.01         0.10679        0.010004        0.010013


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.643      2.3909e+06          288.33          19.921


 TIME FOR THE TIME STEP              201:        0.19843E+03

===============================================================


 INSTANT    0.202000000E+02   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        -0.785026298E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441360E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24719E+01 0.18421E+01
   Friction velocity        uet   :  0.15040E-01 0.18408E+02
   Friction velocity        uk    :  0.15017E-01 0.18408E+02
   Dimensionless distance   yplus :  0.22300E-02 0.97653E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3307
   Nb of faces within the viscous sub-layer     :      27240
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
--------------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24719E+01 0.18421E+01
   Friction velocity        uet   :  0.15040E-01 0.18408E+02
   Friction velocity        uk    :  0.15017E-01 0.18408E+02
   Dimensionless distance   yplus :  0.22300E-02 0.97653E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3307
   Nb of faces within the viscous sub-layer     :      27240
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
---------------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24719E+01 0.18421E+01
   Friction velocity        uet   :  0.15040E-01 0.18408E+02
   Friction velocity        uk    :  0.15017E-01 0.18408E+02
   Dimensionless distance   yplus :  0.22300E-02 0.97653E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3307
   Nb of faces within the viscous sub-layer     :      27240
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69128E+00     520   0.15880E+00   0.72234E+01 0.11882E+02 
c  Velocity[X]                                      0.74870E+00 
c  Velocity[Y]                                      0.12205E+01 
c  Velocity[Z]                                      0.52542E+01 
c  Pressure     0.14665E+00    1572   0.14540E+00   0.32809E+00 0.74384E+01 
c  k            0.26042E-01     206   0.36465E-02   0.37819E-02 0.26314E+02 
c  epsilon      0.36031E+03     159   0.52290E-02   0.86084E+06 0.92426E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.7639e-05                             9
a  epsilon                -0.21957                            18
a  Local Time Step      4.2278e-08                        281685


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8864          5.1068         0.45425         0.11676
v  Velocity[Y]             -3.8327          7.0302         0.39794         0.27601
v  Velocity[Z]             -7.4585          4.9475         -0.1888        0.029887
v  ǁVelocityǁ            0.0012025          9.4943          1.4826          2.1692
v  Pressure                -22.454           29098           18526           15918
v  k                    6.8744e-09         0.82533       0.0074146        0.011588
v  epsilon              6.1243e-05           43976          43.017          7.4057
v  TurbVisc             4.6999e-14         0.16708      0.00054308       0.0080276
v  CourantNb              0.018225           34948          87.803          22.313
v  FourierNb               0.22215      2.3653e+06          217.38          2.7805
v  total_pressure       4.9998e+05       5.291e+05      5.1853e+05      5.1592e+05
v  Local Time Step            0.01        0.030291        0.010001        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2529      2.3841e+06          305.19          25.093


 TIME FOR THE TIME STEP              202:        0.21187E+03

===============================================================


 INSTANT    0.203000000E+02   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        -0.249646011E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441732E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.22268E+01 0.17997E+01
   Friction velocity        uet   :  0.16175E-01 0.30794E+02
   Friction velocity        uk    :  0.16122E-01 0.30794E+02
   Dimensionless distance   yplus :  0.39293E-02 0.10220E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3292
   Nb of faces within the viscous sub-layer     :      26767
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70498E+00     512   0.14841E+00   0.14151E+01 0.51770E+01 
c  Velocity[X]                                      0.35762E+00 
c  Velocity[Y]                                      0.52991E+00 
c  Velocity[Z]                                      0.52753E+00 
c  Pressure     0.98544E-01    1754   0.18965E+00   0.20866E+00 0.18933E+02 
c  k            0.26665E-01     179   0.14929E-02   0.16595E-02 0.18037E+02 
c  epsilon      0.42326E+03     105   0.24776E-02   0.51169E+06 0.14412E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initia   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4645      2.4383e+06          308.34          25.448


 TIME FOR THE TIME STEP              203:        0.20169E+03

===============================================================


 INSTANT    0.204000000E+02   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        -0.716293130E-18
Rough wall               ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4645      2.4383e+06          308.34          25.448


 TIME FOR THE TIME STEP              203:        0.20872E+03

===============================================================


 INSTANT    0.204000000E+02   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        -0.716293130E-18
Rough wall                ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4645      2.4383e+06          308.34          25.448


 TIME FOR THE TIME STEP              203:        0.20852E+03

===============================================================


 INSTANT    0.204000000E+02   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        -0.716293130E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441774E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.22969E+01 0.17472E+01
   Friction velocity        uet   :  0.21224E-01 0.29988E+02
   Friction velocity        uk    :  0.21144E-01 0.29988E+02
   Dimensionless distance   yplus :  0.38265E-02 0.10550E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3343
   Nb of faces within the viscous sub-layer     :      26391
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68078E+00     477   0.15331E+00   0.11316E+01 0.46630E+01 
c  Velocity[X]                                      0.21584E+00 
c  Velocity[Y]                                      0.37517E+00 
c  Velocity[Z]                                      0.54062E+00 
c  Pressure     0.11233E+00    1633   0.15324E+00   0.22671E+00 0.10433E+02 
c  k            0.26582E-01     182   0.70695E-03   0.36983E-03 0.84291E+01 
c  epsilon      0.39891E+03     129   0.61280E-03   0.37983E+05 0.36652E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00048873                            54
a  epsilon                 -1.8577                           110
a  Local Time Step      4.2278e-08                        281644


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9418          4.6181         0.46466         0.11562
v  Velocity[Y]             -3.9007          6.7949         0.39873         0.27465
v  Velocity[Z]             -7.3087           4.836        -0.24822       0.0021203
v  ǁVelocityǁ           0.00041107          8.9034          1.5428          2.1902
v  Pressure                  -1221           21825           14767           11705
v  k                    5.2954e-09         0.51872       0.0063011        0.011599
v  epsilon              2.4972e-06           12456          25.066          6.1577
v  TurbVisc             3.6274e-14         0.16883      0.00053983       0.0083988
v  CourantNb              0.047413           66354          91.789          22.915
v  FourierNb               0.22203      2.3653e+06          217.35          2.7824
v  total_pressure       4.9878e+05      5.2183e+05      5.1477e+05       5.117e+05
v  Local Time Step            0.01        0.020916        0.010001        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6103       2.403e+06          309.14          25.697


 TIME FOR THE TIME STEP              204:        0.19834E+03

===============================================================


 INSTANT    0.205000000E+02   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        -0.311620543E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441761E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.22894E+01 0a  epsilon                 -11.119                           200
a  Local Time Step      4.2278e-08                        281651


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.0182          4.5308         0.46694         0.11411
v  Velocity[Y]             -4.0203          7.0771         0.38758         0.27012
v  Velocity[Z]              -7.302          4.8791        -0.26474      -0.0060299
v  ǁVelocityǁ            0.0031705          8.6709           1.564          2.1767
v  Pressure                -1775.4           21747           14564           11634
v  k                    6.4904e-09         0.53833       0.00628a  epsilon                 -11.119                           200
a  Local Time Step      4.2278e-08                        281651


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.0182          4.5308         0.46694         0.11411
v  Velocity[Y]             -4.0203          7.0771         0.38758         0.27012
v  Velocity[Z]              -7.302          4.8791        -0.26474      -0.0060299
v  ǁVelocityǁ            0.0031705          8.6709           1.564          2.1767
v  Pressure                -1775.4           21747           14564           11634
v  k                    6.4904e-09         0.53833       0.006287a  epsilon                 -11.119                           200
a  Local Time Step      4.2278e-08                        281651


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.0182          4.5308         0.46694         0.11411
v  Velocity[Y]             -4.0203          7.0771         0.38758         0.27012
v  Velocity[Z]              -7.302          4.8791        -0.26474      -0.0060299
v  ǁVelocityǁ            0.0031705          8.6709           1.564          2.1767
v  Pressure                -1775.4           21747           14564           11634
v  k                    6.4904e-09         0.53833       0.0062877        0.011638
v  epsilon              6.6951e-06           13085          23.723          6.1233
v  TurbVisc             3.9824e-14         0.16882      0.00056018       0.0085091
v  CourantNb              0.036704           67626          91.891          23.056
v  FourierNb               0.22193      2.3653e+06          217.37          2.7851
v  total_pressure       4.9822e+05      5.2175e+05      5.1456e+05      5.1163e+05
v  Local Time Step            0.01        0.023008        0.010001        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6294      2.3691e+06          309.26          25.842


 TIME FOR THE TIME STEP              205:        0.18245E+03

===============================================================


 INSTANT    0.206000000E+02   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        -0.590311305E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441755E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24432E+01 0.17781E+01
   Friction velocity        uet   :  0.23438E-01 0.31076E+02
   Friction velocity        uk    :  0.23194E-01 0.31076E+02
   Dimensionless distance   yplus :  0.39653E-02 0.10717E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3404
   Nb of faces within the viscous sub-layer     :      26087
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65535E+00     467   0.16347E+00   0.69821E+00 0.36835E+01 
c  Velocity[X]                                      0.16586E+00 
c  Velocity[Y]                                      0.26927E+00 
c  Velocity[Z]                                      0.26308E+00 
c  Pressure     0.83654E-01    1538   0.91850E-01   0.15525E+00 0.39126E+01 
c  k            0.26249E-01     174   0.52024E-03   0.14801E-03 0.53111E+01 
c  epsilon      0.32347E+03     125   0.69824E-03   0.17202E+05 0.25984E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00059618                            53
a  epsilon                -0.72324                            98
a  Local Time Step      4.2278e-08                        281671


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.0658          4.4486         0.47103         0.11392
v  Velocity[Y]             -4.1466          7.0014         0.37724         0.26884
v  Velocity[Z]             -7.3638          4.8461        -0.26817      -0.0056725
v  ǁVelocityǁ             0.001401          8.5674          1.5884          2.1759
v  Pressure                -1640.8           22333           14991           12151
v  k                    3.2204e-09         0.52723        0.006574         0.01172
v  epsilon              2.4806e-06           13718          25.519          6.2542
v  TurbVisc             4.9766e-14         0.16882      0.00057195       0.0085837
v  CourantNb             0.0050726           70547          92.974          23.211
v  FourierNb               0.22189      2.3653e+06          217.38           2.787
v  total_pressure       4.9836e+05      5.2233e+05      5.1499e+05      5.1215e+05
v  Local Time Step            0.01        0.025309        0.010001        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5959      2.3963e+06          310.36          25.99   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3447
   Nb of faces within the viscous sub-layer     :      25961
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65686E+00     444   0.16452E+00   0.58712E+00 0.33662E+01 
c  Velocity[X]                                      0.14398E+00 
c  Velocity[Y]                                      0.23172E+00 
c  Velocity[Z]                 ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3447
   Nb of faces within the viscous sub-layer     :      25961
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65686E+00     444   0.16452E+00   0.58712E+00 0.33662E+01 
c  Velocity[X]                                      0.14398E+00 
c  Velocity[Y]                                      0.23172E+00 
c  Velocity[Z]                  ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3447
   Nb of faces within the viscous sub-layer     :      25961
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65686E+00     444   0.16452E+00   0.58712E+00 0.33662E+01 
c  Velocity[X]                                      0.14398E+00 
c  Velocity[Y]                                      0.23172E+00 
c  Velocity[Z]                                      0.21142E+00 
c  Pressure     0.73299E-01    1521   0.77804E-01   0.13128E+00 0.40371E+01 
c  k            0.26192E-01     164   0.43630E-03   0.10350E-03 0.44317E+01 
c  epsilon      0.29952E+03      95   0.73768E-03   0.13536E+05 0.23010E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00056344                            24
a  epsilon                 -3.6129                            31
a  Local Time Step      4.2278e-08                        281659


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.1352           4.434         0.47478         0.11417
v  Velocity[Y]             -4.2392          7.1091         0.36884         0.26965
v  Velocity[Z]              -7.382          4.8186        -0.26705      -0.0030495
v  ǁVelocityǁ           0.00098065          8.4973          1.6113          2.1831
v  Pressure                -1364.6           23094           15555           12712
v  k                    1.1403e-08         0.54015       0.0067051         0.01178
v  epsilon              1.1249e-06           16647          26.708          6.3261
v  TurbVisc              6.473e-14         0.16882       0.0005834       0.0086361
v  CourantNb              0.067408           68435          94.803          23.381
v  FourierNb               0.22188      2.3653e+06           217.4          2.7882
v  total_pressure       4.9864e+05      5.2309e+05      5.1556e+05      5.1271e+05
v  Local Time Step            0.01         0.02784        0.010001        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6177      2.4162e+06          312.21          26.169


 TIME FOR THE TIME STEP              207:        0.18887E+03

===============================================================


 INSTANT    0.208000000E+02   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        -0.487495967E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441302E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23915E+01 0.17665E+01
   Friction velocity        uet   :  0.88326E-02 0.36194E+02
   Friction velocity        uk    :  0.88045E-02 0.36194E+02
   Dimensionless distance   yplus :  0.46184E-02 0.10661E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3472
   Nb of faces within the viscous sub-layer     :      25820
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66149E+00     446   0.16680E+00   0.50130E+00 0.30962E+01 
c  Velocity[X]                                      0.11433E+00 
c  Velocity[Y]                                      0.21573E+00 
c  Velocity[Z]                                      0.17124E+00 
c  Pressure     0.67551E-01    1513   0.68358E-01   0.11702E+00 0.28784E+01 
c  k            0.26172E-01     161   0.47121E-03   0.12182E-03 0.47930E+01 
c  epsilon      0.27885E+03     114   0.65199E-03   0.16824E+05 0.25069E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00060969                            25
a  epsilon                 -12.489                            34
a  Local Time Step      4.2278e-08                        281644


  ** Computed fields on cells
     -------------- ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.432506213E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441312E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+ ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.432506213E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441312E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+0 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.432506213E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441312E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24019E+01 0.17590E+01
   Friction velocity        uet   :  0.12604E-01 0.37935E+02
   Friction velocity        uk    :  0.12543E-01 0.37935E+02
   Dimensionless distance   yplus :  0.48405E-02 0.10674E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3526
   Nb of faces within the viscous sub-layer     :      25718
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66520E+00     449   0.17239E+00   0.44041E+00 0.28910E+01 
c  Velocity[X]                                      0.98887E-01 
c  Velocity[Y]                                      0.19207E+00 
c  Velocity[Z]                                      0.14945E+00 
c  Pressure     0.62093E-01    1441   0.60894E-01   0.10444E+00 0.17988E+01 
c  k            0.26149E-01     167   0.40802E-03   0.10076E-03 0.43534E+01 
c  epsilon      0.26254E+03     122   0.69999E-03   0.12983E+05 0.21945E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00058299                            27
a  epsilon                -0.63212                            34
a  Local Time Step      4.2278e-08                        281642


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.2437          4.5775           0.483         0.11461
v  Velocity[Y]             -4.3961          7.5343         0.36068           0.271
v  Velocity[Z]              -7.249          4.7926        -0.26859      -0.0012224
v  ǁVelocityǁ           0.00076328           8.261          1.6514          2.2014
v  Pressure                -1169.5           24176           16302           13331
v  k                    4.8259e-09         0.61211       0.0070491        0.011896
v  epsilon              2.9611e-05           22675          30.111          6.5195
v  TurbVisc             8.0903e-14         0.16882      0.00059888       0.0086928
v  CourantNb              0.058898           82568          97.968          23.694
v  FourierNb               0.22196      2.3653e+06          217.44          2.7902
v  total_pressure       4.9883e+05      5.2418e+05       5.163e+05      5.1333e+05
v  Local Time Step            0.01         0.03038        0.010001        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6344       2.419e+06          315.41          26.484


 TIME FOR THE TIME STEP              209:        0.18214E+03

===============================================================


 INSTANT    0.210000000E+02   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        -0.166683189E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441309E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23677E+01 0.18287E+01
   Friction velocity        uet   :  0.13962E-01 0.37064E+02
   Friction velocity        uk    :  0.13889E-01 0.37064E+02
   Dimensionless distance   yplus :  0.47294E-02 0.10632E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3569
   Nb of faces within the viscous sub-layer   v  Velocity[X]             -2.3416          4.6589         0.48582         0.11451
v  Velocity[Y]               -4.48           7.705         0.36022         0.27113
v  Velocity[Z]             -7.1015          4.7517        -0.27017      -0.0016834
v  ǁVelocityǁ           0.00027696           8.391          1.6678           2.208
v  Pressure                  -1217           24514           16497           13466
v  k                    1.2977e-08         0.58389       0.0072471        0.011941
v  epsilon              1.9972e-06           16040          30.786          6.6157
v  TurbVisc             8.7807e-14         0.16882      0.00060265       0.0087062
v  CourantNb              0.013288           82353          98.938          23.823
v  FourierNb               0.22199      2.3653e+06          217.44          2.7906
v  totalv  Velocity[X]             -2.3416          4.6589         0.48582         0.11451
v  Velocity[Y]               -4.48           7.705         0.36022         0.27113
v  Velocity[Z]             -7.1015          4.7517        -0.27017      -0.0016834
v  ǁVelocityǁ           0.00027696           8.391          1.6678           2.208
v  Pressure                  -1217           24514           16497           13466
v  k                    1.2977e-08         0.58389       0.0072471        0.011941
v  epsilon              1.9972e-06           16040          30.786          6.6157
v  TurbVisc             8.7807e-14         0.16882      0.00060265       0.0087062
v  CourantNb              0.013288           82353          98.938          23.823
v  FourierNb               0.22199      2.3653e+06          217.44          2.7906
v  total_v  Velocity[X]             -2.3416          4.6589         0.48582         0.11451
v  Velocity[Y]               -4.48           7.705         0.36022         0.27113
v  Velocity[Z]             -7.1015          4.7517        -0.27017      -0.0016834
v  ǁVelocityǁ           0.00027696           8.391          1.6678           2.208
v  Pressure                  -1217           24514           16497           13466
v  k                    1.2977e-08         0.58389       0.0072471        0.011941
v  epsilon              1.9972e-06           16040          30.786          6.6157
v  TurbVisc             8.7807e-14         0.16882      0.00060265       0.0087062
v  CourantNb              0.013288           82353          98.938          23.823
v  FourierNb               0.22199      2.3653e+06          217.44          2.7906
v  total_pressure       4.9878e+05      5.2451e+05       5.165e+05      5.1347e+05
v  Local Time Step            0.01         0.02855        0.010001        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6415      2.4191e+06          316.38          26.614


 TIME FOR THE TIME STEP              210:        0.17929E+03

===============================================================


 INSTANT    0.211000000E+02   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        -0.512965922E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441318E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23745E+01 0.17835E+01
   Friction velocity        uet   :  0.11566E-01 0.35030E+02
   Friction velocity        uk    :  0.11563E-01 0.35030E+02
   Dimensionless distance   yplus :  0.44698E-02 0.10636E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3601
   Nb of faces within the viscous sub-layer     :      25526
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66853E+00     433   0.17104E+00   0.40926E+00 0.27726E+01 
c  Velocity[X]                                      0.94022E-01 
c  Velocity[Y]                                      0.18509E+00 
c  Velocity[Z]                                      0.13015E+00 
c  Pressure     0.55108E-01    1336   0.50286E-01   0.88275E-01 0.91994E+00 
c  k            0.26198E-01     167   0.44416E-03   0.80712E-04 0.38836E+01 
c  epsilon      0.24557E+03     142   0.52100E-03   0.12820E+05 0.21133E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00058788                            86
a  epsilon                -0.89566                            79
a  Local Time Step      4.2278e-08                        281671


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.3864          4.7276         0.48842         0.11416
v  Velocity[Y]             -4.5761          8.1409         0.36142         0.27112
v  Velocity[Z]             -7.1523          4.7293        -0.27322      -0.0022148
v  ǁVelocityǁ           0.00048531          8.8532          1.6833          2.2129
v  Pressure                -1278.6           24792           16645           13571
v  k                      1.04e-08         0.66154       0.0073336        0.011968
v  epsilon               4.258e-06           21167           31.56          6.6663
v  TurbVisc              8.559e-14         0.16882      0.00060794       0.0087144
v  CourantNb              0.028173           81298          99.752          23.936
v  FourierNb               0.22203      2.3653e+06          217.46           2.791
v  total_pressure       4.9872e+05      5.2479e+05      5.1664e+05      5.1357e+05
v  Local Time Step            0.01         0.03007        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6124      2.4219e+06          317.21          26.727


 TIME FOR THE TIME STEP              211:        0.17533E+03

===============================================================


 INSTANT    0.212000000E+02   TIME STEP NUMBER             212
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66968E+00     436   0.17572E+00   0.42307E+00 0.28134E+01 
c  Velocity[X]                                      0.97099E-01 
c  Velocity[Y]                                      0.19025E+00 
c  Velocity[Z]                                      0.13572E+00 
c  Pressure     0.53366E-01    1353   0.46613E-01   0.83703E-01 0.82169E+00 
c  k            0.26214E-01     163   0.38983E-03   0.97220E-04 0.42556E+01 
c  epsilon      0.23745E+03     110   0.64769E-03   0.12627E+05 0.20684E+02 
----------------------------------------------------------------------      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66968E+00     436   0.17572E+00   0.42307E+00 0.28134E+01 
c  Velocity[X]                                      0.97099E-01 
c  Velocity[Y]                                      0.19025E+00 
c  Velocity[Z]                                      0.13572E+00 
c  Pressure     0.53366E-01    1353   0.46613E-01   0.83703E-01 0.82169E+00 
c  k            0.26214E-01     163   0.38983E-03   0.97220E-04 0.42556E+01 
c  epsilon      0.23745E+03     110   0.64769E-03   0.12627E+05 0.20684E+02 
-----------------------------------------------------------------------      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66968E+00     436   0.17572E+00   0.42307E+00 0.28134E+01 
c  Velocity[X]                                      0.97099E-01 
c  Velocity[Y]                                      0.19025E+00 
c  Velocity[Z]                                      0.13572E+00 
c  Pressure     0.53366E-01    1353   0.46613E-01   0.83703E-01 0.82169E+00 
c  k            0.26214E-01     163   0.38983E-03   0.97220E-04 0.42556E+01 
c  epsilon      0.23745E+03     110   0.64769E-03   0.12627E+05 0.20684E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00057354                            99
a  epsilon                -0.33391                            95
a  Local Time Step      4.2278e-08                        281693


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.4178          4.7914         0.49046         0.11388
v  Velocity[Y]             -4.5988          8.0803         0.36245         0.27098
v  Velocity[Z]               -7.22          4.5733        -0.27588      -0.0024474
v  ǁVelocityǁ           0.00065133          8.7445          1.6972          2.2172
v  Pressure                -1333.3           25045           16783           13673
v  k                    9.4624e-10         0.56999       0.0074944        0.012003
v  epsilon              1.9422e-05           20632          32.898          6.7461
v  TurbVisc             8.8293e-14         0.16883      0.00061124        0.008719
v  CourantNb             0.0090361           78299          100.42          24.032
v  FourierNb               0.22206      2.3653e+06          217.46          2.7911
v  total_pressure       4.9867e+05      5.2504e+05      5.1678e+05      5.1367e+05
v  Local Time Step            0.01        0.027385        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6085      2.4211e+06          317.88          26.823


 TIME FOR THE TIME STEP              212:        0.17381E+03

===============================================================


 INSTANT    0.213000000E+02   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        -0.618069277E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441260E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.22321E+01 0.18233E+01
   Friction velocity        uet   :  0.23825E-01 0.30350E+02
   Friction velocity        uk    :  0.23822E-01 0.30350E+02
   Dimensionless distance   yplus :  0.38727E-02 0.10461E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3670
   Nb of faces within the viscous sub-layer     :      25310
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67044E+00     441   0.17428E+00   0.40866E+00 0.27611E+01 
c  Velocity[X]                                      0.97310E-01 
c  Velocity[Y]                                      0.16923E+00 
c  Velocity[Z]                                      0.14212E+00 
c  Pressure     0.52605E-01    1333   0.44634E-01   0.80987E-01 0.86768E+00 
c  k            0.26268E-01     159   0.38165E-03   0.79362E-04 0.38399E+01 
c  epsilon      0.23605E+03     112   0.66559E-03   0.10191E+05 0.18313E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00051065                            26
a  epsilon                 -2.3795                            44
a  Local Time Step      4.2278e-08                        281703


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5012          4.8382          0.4913         0.11384
v  Velocity[Y]             -4.6387          8.4984         0.36371    Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.373878493E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441284E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum   Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.373878493E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441284E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum    Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.373878493E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441284E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.21866E+01 0.18381E+01
   Friction velocity        uet   :  0.94396E-02 0.29406E+02
   Friction velocity        uk    :  0.94357E-02 0.29406E+02
   Dimensionless distance   yplus :  0.37522E-02 0.10361E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3708
   Nb of faces within the viscous sub-layer     :      25228
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67141E+00     440   0.18172E+00   0.39833E+00 0.27222E+01 
c  Velocity[X]                                      0.89149E-01 
c  Velocity[Y]                                      0.16328E+00 
c  Velocity[Z]                                      0.14590E+00 
c  Pressure     0.52491E-01    1338   0.43682E-01   0.79517E-01 0.83909E+00 
c  k            0.26276E-01     166   0.35894E-03   0.81788E-04 0.38944E+01 
c  epsilon      0.23033E+03     115   0.74203E-03   0.11702E+05 0.19435E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00052441                            28
a  epsilon                -0.41275                            28
a  Local Time Step      4.2278e-08                        281706


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.4837           4.895         0.49284         0.11384
v  Velocity[Y]             -4.6245          8.3101          0.3634         0.27124
v  Velocity[Z]             -7.1994          4.5925        -0.27954      -0.0024932
v  ǁVelocityǁ           0.00086254          8.9998          1.7169          2.2236
v  Pressure                -1403.1           25550           17098           13913
v  k                    1.0754e-08         0.61879       0.0077117        0.012054
v  epsilon              7.8155e-05           18682          35.362          6.8528
v  TurbVisc             7.3261e-14         0.16883      0.00061823       0.0087263
v  CourantNb               0.01685           71811           101.5          24.188
v  FourierNb               0.22213      2.3653e+06          217.48          2.7919
v  total_pressure        4.986e+05      5.2555e+05       5.171e+05      5.1391e+05
v  Local Time Step            0.01        0.027661        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6317      2.4116e+06          318.98           26.98


 TIME FOR THE TIME STEP              214:        0.17483E+03

===============================================================


 INSTANT    0.215000000E+02   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        -0.148281013E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441259E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.21928E+01 0.18556E+01
   Friction velocity        uet   :  0.26067E-01 0.28521E+02
   Friction velocity        uk    :  0.25942E-01 0.28521E+02
   Dimensionless distance   yplus :  0.36394E-02 0.10397E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3740
   Nb of faces within the viscous sub-layer     :      25155
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residuav  Pressure                -1450.7           25771           17247           14022
v  k                     1.011e-08          0.6185        0.007747        0.012085
v  epsilon              5.7534e-06           19984          34.941          6.9021
v  TurbVisc             6.7916e-14         0.16883      0.00062094       0.0087294
v  CourantNb              0.060538           70061          101.82          24.243
v  FourierNb               0.22217      2.3653e+06          217.48          2.7923
v  total_pressure       4.9855e+05      5.2577e+05      5.1725e+05      5.1402e+05
v  Local Time Step            0.01        0.028531        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  ----------v  Pressure                -1450.7           25771           17247           14022
v  k                     1.011e-08          0.6185        0.007747        0.012085
v  epsilon              5.7534e-06           19984          34.941          6.9021
v  TurbVisc             6.7916e-14         0.16883      0.00062094       0.0087294
v  CourantNb              0.060538           70061          101.82          24.243
v  FourierNb               0.22217      2.3653e+06          217.48          2.7923
v  total_pressure       4.9855e+05      5.2577e+05      5.1725e+05      5.1402e+05
v  Local Time Step            0.01        0.028531        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  -----------v  Pressure                -1450.7           25771           17247           14022
v  k                     1.011e-08          0.6185        0.007747        0.012085
v  epsilon              5.7534e-06           19984          34.941          6.9021
v  TurbVisc             6.7916e-14         0.16883      0.00062094       0.0087294
v  CourantNb              0.060538           70061          101.82          24.243
v  FourierNb               0.22217      2.3653e+06          217.48          2.7923
v  total_pressure       4.9855e+05      5.2577e+05      5.1725e+05      5.1402e+05
v  Local Time Step            0.01        0.028531        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6478      2.4089e+06          319.31          27.036


 TIME FOR THE TIME STEP              215:        0.17797E+03

===============================================================


 INSTANT    0.216000000E+02   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        -0.159905631E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441248E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.22020E+01 0.18613E+01
   Friction velocity        uet   :  0.23483E-01 0.27632E+02
   Friction velocity        uk    :  0.23365E-01 0.27632E+02
   Dimensionless distance   yplus :  0.35258E-02 0.10321E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3761
   Nb of faces within the viscous sub-layer     :      25068
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67248E+00     436   0.17397E+00   0.37493E+00 0.26351E+01 
c  Velocity[X]                                      0.95297E-01 
c  Velocity[Y]                                      0.16548E+00 
c  Velocity[Z]                                      0.11415E+00 
c  Pressure     0.52169E-01    1304   0.40507E-01   0.76990E-01 0.68938E+00 
c  k            0.26381E-01     170   0.37809E-03   0.59120E-04 0.33040E+01 
c  epsilon      0.23377E+03     113   0.78666E-03   0.77203E+04 0.15475E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00059505                            12
a  epsilon                -0.36636                            24
a  Local Time Step      4.2278e-08                        281712


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.4581          4.9733         0.49379         0.11428
v  Velocity[Y]             -4.6131          7.9874         0.36412         0.27151
v  Velocity[Z]             -7.3514          4.5029        -0.28293      -0.0022109
v  ǁVelocityǁ            0.0018288          8.6363          1.7311          2.2281
v  Pressure                -1511.2           25968           17381           14119
v  k                    9.7028e-09         0.67308       0.0078352        0.012111
v  epsilon              5.6625e-05           23189          35.839          6.9563
v  TurbVisc             6.3874e-14         0.16883      0.00062413       0.0087331
v  CourantNb              0.022629           66951          102.12          24.283
v  FourierNb               0.22223      2.3653e+06          217.49          2.7927
v  total_pressure       4.9849e+05      5.2597e+05      5.1738e+05      5.1412e+05
v  Local Time Step            0.01        0.031384        0.010001        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6374      2.4088e+06          319.61          27.076


 TIME FOR THE TIME STEP              216:        0.17051E+03

===============================================================


 INSTANT    0.217000000E+02   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         0.270359594E-17
Rough wall                6 c  Velocity[X]                                      0.89927E-01 
c  Velocity[Y]                                      0.15758E+00 
c  Velocity[Z]                                      0.11268E+00 
c  Pressure     0.49458E-01    1274   0.36910E-01   0.72227E-01 0.62843E+00 
c  k            0.26374E-01     147   0.38501E-03   0.70370E-04 0.36018E+01 
c  epsilon      0.22723E+03      96   0.92817E-03   0.10792E+05 0.18253E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00056996                            13
a  epsilon                 -18.697 c  Velocity[X]                                      0.89927E-01 
c  Velocity[Y]                                      0.15758E+00 
c  Velocity[Z]                                      0.11268E+00 
c  Pressure     0.49458E-01    1274   0.36910E-01   0.72227E-01 0.62843E+00 
c  k            0.26374E-01     147   0.38501E-03   0.70370E-04 0.36018E+01 
c  epsilon      0.22723E+03      96   0.92817E-03   0.10792E+05 0.18253E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00056996                            13
a  epsilon                 -18.697  c  Velocity[X]                                      0.89927E-01 
c  Velocity[Y]                                      0.15758E+00 
c  Velocity[Z]                                      0.11268E+00 
c  Pressure     0.49458E-01    1274   0.36910E-01   0.72227E-01 0.62843E+00 
c  k            0.26374E-01     147   0.38501E-03   0.70370E-04 0.36018E+01 
c  epsilon      0.22723E+03      96   0.92817E-03   0.10792E+05 0.18253E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00056996                            13
a  epsilon                 -18.697                            27
a  Local Time Step      4.2278e-08                        281716


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5123          4.9849         0.49396         0.11458
v  Velocity[Y]             -4.6009          7.4711         0.36543         0.27164
v  Velocity[Z]              -7.372          4.4805        -0.28512      -0.0019215
v  ǁVelocityǁ            0.0016341          8.3867          1.7374          2.2297
v  Pressure                -1577.2           26146           17503           14207
v  k                    9.3055e-09         0.62172        0.007929        0.012133
v  epsilon              2.1079e-06           20091          36.807          6.9949
v  TurbVisc             6.1426e-14         0.16883       0.0006292       0.0087367
v  CourantNb              0.021616           66377          102.53          24.322
v  FourierNb               0.22231      2.3653e+06           217.5           2.793
v  total_pressure       4.9842e+05      5.2615e+05       5.175e+05      5.1421e+05
v  Local Time Step            0.01        0.034523        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6395      2.4087e+06          320.02          27.115


 TIME FOR THE TIME STEP              217:        0.17275E+03

===============================================================


 INSTANT    0.218000000E+02   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         0.234568880E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441218E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.22623E+01 0.18886E+01
   Friction velocity        uet   :  0.19936E-01 0.27854E+02
   Friction velocity        uk    :  0.19919E-01 0.27854E+02
   Dimensionless distance   yplus :  0.35541E-02 0.10250E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3799
   Nb of faces within the viscous sub-layer     :      24956
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67467E+00     432   0.18731E+00   0.36922E+00 0.26105E+01 
c  Velocity[X]                                      0.92129E-01 
c  Velocity[Y]                                      0.15344E+00 
c  Velocity[Z]                                      0.12366E+00 
c  Pressure     0.48837E-01    1234   0.33672E-01   0.70710E-01 0.54972E+00 
c  k            0.26428E-01     185   0.29136E-03   0.47548E-04 0.29582E+01 
c  epsilon      0.23015E+03     144   0.57042E-03   0.58450E+04 0.13398E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00063349                            13
a  epsilon                 -2.3707                            20
a  Local Time Step      4.2278e-08                        281712


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.4958          5.0417          0.4948         0.11485
v  Velocity[Y]             -4.5746          7.4146         0.36753         0.27197
v  Velocity[Z]             -7.3301          4.4543        -0.28659      -0.0016763
v  ǁVelocityǁ            0.0010941          8.3273          1.7443          2.2311
v  Pressure                -1654.9           26299           17606           14282
v  k                    8.9041e-09         0.63735      Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.22962E+01 0.18978E+01
   Friction velocity        uet   :  0.16210E-01 0.28216E+02
   Friction velocity        uk    :  0.16088E-01 0.28216E+02
   Dimensionless distance   yplus :  0.36004E-02 0.10249E+02
   --Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.22962E+01 0.18978E+01
   Friction velocity        uet   :  0.16210E-01 0.28216E+02
   Friction velocity        uk    :  0.16088E-01 0.28216E+02
   Dimensionless distance   yplus :  0.36004E-02 0.10249E+02
   ---Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.22962E+01 0.18978E+01
   Friction velocity        uet   :  0.16210E-01 0.28216E+02
   Friction velocity        uk    :  0.16088E-01 0.28216E+02
   Dimensionless distance   yplus :  0.36004E-02 0.10249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3816
   Nb of faces within the viscous sub-layer     :      24912
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67513E+00     433   0.18190E+00   0.35796E+00 0.25680E+01 
c  Velocity[X]                                      0.86306E-01 
c  Velocity[Y]                                      0.15121E+00 
c  Velocity[Z]                                      0.12044E+00 
c  Pressure     0.44963E-01    1229   0.29836E-01   0.64611E-01 0.49795E+00 
c  k            0.26440E-01     175   0.34677E-03   0.56774E-04 0.32297E+01 
c  epsilon      0.22690E+03     112   0.43045E-03   0.60807E+04 0.13599E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00031689                            23
a  epsilon                 -32.833                            42
a  Local Time Step      4.2278e-08                        281719


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5387          5.0312         0.49481         0.11497
v  Velocity[Y]             -4.5922          7.0912         0.36924         0.27203
v  Velocity[Z]              -7.309          4.4582          -0.288      -0.0016023
v  ǁVelocityǁ            0.0024356          8.2811          1.7516          2.2329
v  Pressure                -1718.4           26433           17697           14350
v  k                    8.6244e-09         0.62725       0.0080603        0.012175
v  epsilon              3.3015e-06           20721          37.457           7.081
v  TurbVisc             5.5966e-14         0.16883      0.00063357       0.0087412
v  CourantNb             0.0099996           63350          103.29          24.385
v  FourierNb               0.22247      2.3653e+06           217.5          2.7932
v  total_pressure       4.9828e+05      5.2643e+05       5.177e+05      5.1435e+05
v  Local Time Step            0.01        0.041772        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6024      2.4028e+06          320.78          27.179


 TIME FOR THE TIME STEP              219:        0.17018E+03

===============================================================


 INSTANT    0.220000000E+02   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        -0.511371876E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441261E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23139E+01 0.18987E+01
   Friction velocity        uet   :  0.19333E-01 0.26258E+02
   Friction velocity        uk    :  0.19330E-01 0.26258E+02
   Dimensionless distance   yplus :  0.33506E-02 0.10287E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3838
   Nb of faces within the viscous sub-layer     :      24852
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67612E+00     434   0.18850E+00   0.31578E+00 0.24095E+01 
c  Velocity[X]                                      0.75239E-01 
c  Velocity[Y]                                      0.13317E+00 
c  Velocity[Z]     v  CourantNb              0.086523           61397          103.66          24.425
v  FourierNb               0.22253      2.3653e+06           217.5          2.7938
v  total_pressure       4.9822e+05      5.2654e+05      5.1776e+05       5.144e+05
v  Local Time Step            0.01        0.043462        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6263      2.3989e+06          321.15          27.219


 TIME FOR THE TIME STEP              220:        0.16482E+03

===============================================================


 INSTANT    0.221000000E+02   TIME STEP NUMBER             221
 ==v  CourantNb              0.086523           61397          103.66          24.425
v  FourierNb               0.22253      2.3653e+06           217.5          2.7938
v  total_pressure       4.9822e+05      5.2654e+05      5.1776e+05       5.144e+05
v  Local Time Step            0.01        0.043462        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6263      2.3989e+06          321.15          27.219


 TIME FOR THE TIME STEP              220:        0.16942E+03

===============================================================


 INSTANT    0.221000000E+02   TIME STEP NUMBER             221
 ===v  CourantNb              0.086523           61397          103.66          24.425
v  FourierNb               0.22253      2.3653e+06           217.5          2.7938
v  total_pressure       4.9822e+05      5.2654e+05      5.1776e+05       5.144e+05
v  Local Time Step            0.01        0.043462        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6263      2.3989e+06          321.15          27.219


 TIME FOR THE TIME STEP              220:        0.17100E+03

===============================================================


 INSTANT    0.221000000E+02   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        -0.769069837E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441258E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23230E+01 0.19116E+01
   Friction velocity        uet   :  0.24602E-01 0.26103E+02
   Friction velocity        uk    :  0.24557E-01 0.26103E+02
   Dimensionless distance   yplus :  0.33308E-02 0.10311E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3857
   Nb of faces within the viscous sub-layer     :      24809
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67654E+00     434   0.18895E+00   0.29821E+00 0.23398E+01 
c  Velocity[X]                                      0.72277E-01 
c  Velocity[Y]                                      0.12867E+00 
c  Velocity[Z]                                      0.97265E-01 
c  Pressure     0.40936E-01    1194   0.26329E-01   0.58065E-01 0.33339E+00 
c  k            0.26518E-01     162   0.26886E-03   0.53064E-04 0.31162E+01 
c  epsilon      0.22788E+03     142   0.59854E-03   0.11300E+05 0.18034E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021479                            17
a  epsilon                 -24.916                            26
a  Local Time Step      4.2278e-08                        281706


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5525          5.0062         0.49574           0.115
v  Velocity[Y]             -4.5785          6.8424         0.37186           0.271
v  Velocity[Z]             -7.2994          4.4292        -0.29163      -0.0016719
v  ǁVelocityǁ            0.0044446          8.2283          1.7653           2.236
v  Pressure                -1810.9           26623           17818           14444
v  k                    1.0154e-08         0.68413       0.0082159         0.01221
v  epsilon              2.9105e-05           23278          39.046          7.1809
v  TurbVisc             5.3973e-14         0.16883      0.00063705       0.0087449
v  CourantNb                0.0144           61155          104.14          24.463
v  FourierNb               0.22256      2.3653e+06           217.5          2.7939
v  total_pressure       4.9819e+05      5.2662e+05      5.1782e+05      5.1444e+05
v  Local Time Step            0.01        0.043479        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6424      2.3974e+06          321.64          27.257


 TIME FOR THE TIME STEP              221:        0.17282E+03

===============================================================


 INSTANT    0.222000000E+02   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        -0.766411122E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441245E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.0000000c  epsilon      0.23084E+03     106   0.46892E-03   0.59889E+04 0.13096E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001038                           143
a  epsilon                -0.94838                           172
a  Local Time Step      4.2278e-08                        281699


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]           c  epsilon      0.23084E+03     106   0.46892E-03   0.59889E+04 0.13096E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001038                           143
a  epsilon                -0.94838                           172
a  Local Time Step      4.2278e-08                        281699


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            c  epsilon      0.23084E+03     106   0.46892E-03   0.59889E+04 0.13096E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001038                           143
a  epsilon                -0.94838                           172
a  Local Time Step      4.2278e-08                        281699


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5079          5.0243         0.49656         0.11508
v  Velocity[Y]             -4.6123          6.9669         0.37291         0.27091
v  Velocity[Z]             -7.5173          4.5396        -0.29296      -0.0017406
v  ǁVelocityǁ             0.003841          8.2825          1.7715          2.2376
v  Pressure                -1837.8           26696           17862           14481
v  k                    9.1408e-10         0.70258       0.0082325        0.012228
v  epsilon              9.2302e-06           21662          39.035          7.2129
v  TurbVisc             3.2103e-14         0.16883      0.00064031       0.0087465
v  CourantNb              0.040853           61303           104.6          24.491
v  FourierNb               0.22258      2.3653e+06           217.5          2.7939
v  total_pressure       4.9816e+05       5.267e+05      5.1786e+05      5.1448e+05
v  Local Time Step            0.01         0.04347        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6144      2.3945e+06          322.11          27.285


 TIME FOR THE TIME STEP              222:        0.16819E+03

===============================================================


 INSTANT    0.223000000E+02   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        -0.385615110E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441239E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23412E+01 0.19124E+01
   Friction velocity        uet   :  0.16539E-01 0.23563E+02
   Friction velocity        uk    :  0.16520E-01 0.23563E+02
   Dimensionless distance   yplus :  0.30066E-02 0.10265E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3869
   Nb of faces within the viscous sub-layer     :      24728
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67721E+00     435   0.18717E+00   0.28439E+00 0.22816E+01 
c  Velocity[X]                                      0.73338E-01 
c  Velocity[Y]                                      0.11472E+00 
c  Velocity[Z]                                      0.96333E-01 
c  Pressure     0.37589E-01    1156   0.23740E-01   0.52701E-01 0.24961E+00 
c  k            0.26595E-01     167   0.24271E-03   0.46451E-04 0.29108E+01 
c  epsilon      0.22938E+03      98   0.66142E-03   0.57441E+04 0.12706E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00044937                            16
a  epsilon                 -28.649                            24
a  Local Time Step      4.2278e-08                        281695


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.4829          5.0199         0.49692         0.11525
v  Velocity[Y]             -4.7016          6.6573         0.37487         0.27102
v  Velocity[Z]             -7.5152          4.4121        -0.29329      -0.0018286
v  ǁVelocityǁ             0.004145          8.4041          1.7776          2.2389
v  Pressure                -1847.4           26763           17902           14516
v  k                     7.266e-09         0.68194        0.008291        0.012246
v  epsilon              2.2532e-05           21923          39.551          7.2491
v  TurbVisc             4.1793e-14         0.16883      0.00064325       0.0087486
v  CourantNb              0.015283           63221             105          24.524
v  FourierNb               0.22258      2.3653e+06          217.51          2.7943
v  tot   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23588E+01 0.19182E+01
   Friction velocity        uet   :  0.13230E-01 0.22303E+02
   Friction velocity        uk    :  0.13177E-01 0.22303E+02
   Dimensionless distance   yplus :  0.28459E-02 0.10288E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3870
   Nb of faces within the viscous sub-layer     :      24695
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23588E+01 0.19182E+01
   Friction velocity        uet   :  0.13230E-01 0.22303E+02
   Friction velocity        uk    :  0.13177E-01 0.22303E+02
   Dimensionless distance   yplus :  0.28459E-02 0.10288E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3870
   Nb of faces within the viscous sub-layer     :      24695
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23588E+01 0.19182E+01
   Friction velocity        uet   :  0.13230E-01 0.22303E+02
   Friction velocity        uk    :  0.13177E-01 0.22303E+02
   Dimensionless distance   yplus :  0.28459E-02 0.10288E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3870
   Nb of faces within the viscous sub-layer     :      24695
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67765E+00     432   0.18797E+00   0.27918E+00 0.22587E+01 
c  Velocity[X]                                      0.69688E-01 
c  Velocity[Y]                                      0.11408E+00 
c  Velocity[Z]                                      0.95414E-01 
c  Pressure     0.36535E-01    1081   0.23017E-01   0.50980E-01 0.18256E+00 
c  k            0.26633E-01     154   0.27158E-03   0.38604E-04 0.26518E+01 
c  epsilon      0.23215E+03     112   0.52386E-03   0.48365E+04 0.11605E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00027149                            10
a  epsilon                -0.29847                            17
a  Local Time Step      4.2278e-08                        281692


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -2.509          5.0089         0.49763         0.11525
v  Velocity[Y]             -4.6518          6.9688         0.37542         0.27124
v  Velocity[Z]             -7.2875          4.4655        -0.29359      -0.0017594
v  ǁVelocityǁ             0.001534           8.226          1.7826          2.2402
v  Pressure                -1859.6           26815           17930           14540
v  k                    8.8412e-09         0.68738       0.0083595        0.012261
v  epsilon              5.6389e-06           21849          40.095          7.2796
v  TurbVisc              4.966e-14         0.16883      0.00064657       0.0087508
v  CourantNb             0.0043244           63365          105.43          24.548
v  FourierNb               0.22259      2.3653e+06          217.51          2.7946
v  total_pressure       4.9814e+05      5.2682e+05      5.1793e+05      5.1454e+05
v  Local Time Step            0.01        0.041962        0.010002        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6941      2.3934e+06          322.95          27.343


 TIME FOR THE TIME STEP              224:        0.16008E+03

===============================================================


 INSTANT    0.225000000E+02   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        -0.905426264E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441263E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24031E+01 0.19160E+01
   Friction velocity        uet   :  0.16799E-01 0.21387E+02
   Friction velocity        uk    :  0.16788E-01 0.21387E+02
   Dimensionless distance   yplus :  0.27289E-02 0.10279E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3868
   Nb of faces within the viscous sub-layer     :      24668
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67834E+00     433   0.18976E+00   0.27918E+00 0.22578E+01 
c  Velocity[X]                                      0.69830E-01 
c  Velocity[Y]                                      0.11586E+00 
c  Velocity[Z]                                      0.93499E-01 
c  Pressure     0.36835E-01    1113   0.22549E-01   0.51146E-01 0.16922E+00 
c  k            0.26650E-01     149   0.23656E-03   0.45114E-04 0.28639E+01 
c  epsilon      0.22962E+03     106   0.38392E-03   0.62052E+04 0.13088E+02 
--------------------------------------------------------
  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6818      2.3924e+06           323.3          27.368


 TIME FOR THE TIME STEP              225:        0.16428E+03

===============================================================


 INSTANT    0.226000000E+02   TIME STEP NUMBER             226
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet
  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6818      2.3924e+06           323.3          27.368


 TIME FOR THE TIME STEP              225:        0.16367E+03

===============================================================


 INSTANT    0.226000000E+02   TIME STEP NUMBER             226
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet 
  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6818      2.3924e+06           323.3          27.368


 TIME FOR THE TIME STEP              225:        0.16517E+03

===============================================================


 INSTANT    0.226000000E+02   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        -0.254100584E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441289E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24342E+01 0.19171E+01
   Friction velocity        uet   :  0.23161E-01 0.19712E+02
   Friction velocity        uk    :  0.23125E-01 0.19712E+02
   Dimensionless distance   yplus :  0.25152E-02 0.10366E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3867
   Nb of faces within the viscous sub-layer     :      24639
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67851E+00     428   0.18894E+00   0.28930E+00 0.22968E+01 
c  Velocity[X]                                      0.72218E-01 
c  Velocity[Y]                                      0.11387E+00 
c  Velocity[Z]                                      0.10322E+00 
c  Pressure     0.36649E-01    1084   0.22208E-01   0.50710E-01 0.13092E+00 
c  k            0.26683E-01     141   0.27828E-03   0.44208E-04 0.28335E+01 
c  epsilon      0.23286E+03     107   0.44785E-03   0.46342E+04 0.11249E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.000293                             8
a  epsilon                -0.51162                            15
a  Local Time Step      4.2278e-08                        281676


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5792          5.0124         0.49886          0.1153
v  Velocity[Y]             -4.6316          6.8239          0.3772          0.2715
v  Velocity[Z]             -7.3431          4.5578        -0.29411      -0.0016934
v  ǁVelocityǁ            0.0026602           8.289          1.7911          2.2419
v  Pressure                -1894.5           26902           17977           14579
v  k                    1.0949e-08         0.72398       0.0084608        0.012296
v  epsilon              8.1614e-06           22918          40.697          7.3282
v  TurbVisc             4.5249e-14         0.16883      0.00065303       0.0087564
v  CourantNb             0.0089783           68825          106.07          24.587
v  FourierNb               0.22264      2.3653e+06          217.52          2.7959
v  total_pressure       4.9811e+05       5.269e+05      5.1798e+05      5.1458e+05
v  Local Time Step            0.01        0.050072        0.010002        0.010011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7073      2.3882e+06          323.59          27.383


 TIME FOR THE TIME STEP              226:        0.16685E+03

===============================================================


 INSTANT    0.227000000E+02   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        -0.360379198E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441247E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                            -  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0002353                            31
a  epsilon                 -26.714                            54
a  Local Time Step      4.2278e-08                        281674


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -2.583          5.0067           0.499         0.11538
v  Velocity[Y]             -4.6315          6.6906         0.37832         0.27157
v  Velocity[Z]             -7.4529          4.4214         -0.2939      -0.0016042
v  ǁVelocityǁ            0.0034492          8.3805          1.7938          2.2422
v  -  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0002353                            31
a  epsilon                 -26.714                            54
a  Local Time Step      4.2278e-08                        281674


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -2.583          5.0067           0.499         0.11538
v  Velocity[Y]             -4.6315          6.6906         0.37832         0.27157
v  Velocity[Z]             -7.4529          4.4214         -0.2939      -0.0016042
v  ǁVelocityǁ            0.0034492          8.3805          1.7938          2.2422
v  P-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0002353                            31
a  epsilon                 -26.714                            54
a  Local Time Step      4.2278e-08                        281674


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -2.583          5.0067           0.499         0.11538
v  Velocity[Y]             -4.6315          6.6906         0.37832         0.27157
v  Velocity[Z]             -7.4529          4.4214         -0.2939      -0.0016042
v  ǁVelocityǁ            0.0034492          8.3805          1.7938          2.2422
v  Pressure                -1922.4           26926           17986           14586
v  k                    7.1348e-09         0.73604        0.008515        0.012312
v  epsilon              0.00014056           23543          41.034          7.3479
v  TurbVisc             7.6167e-14         0.16883       0.0006581       0.0087596
v  CourantNb             0.0079972           71187          106.32          24.605
v  FourierNb               0.22268      2.3653e+06          217.53          2.7962
v  total_pressure       4.9808e+05      5.2693e+05      5.1799e+05      5.1459e+05
v  Local Time Step            0.01        0.055079        0.010002        0.010012


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6196      2.3834e+06          323.84          27.401


 TIME FOR THE TIME STEP              227:        0.16254E+03

===============================================================


 INSTANT    0.228000000E+02   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        -0.546695479E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441262E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24828E+01 0.19099E+01
   Friction velocity        uet   :  0.19239E-01 0.19110E+02
   Friction velocity        uk    :  0.19023E-01 0.19110E+02
   Dimensionless distance   yplus :  0.24385E-02 0.10342E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3875
   Nb of faces within the viscous sub-layer     :      24590
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67947E+00     426   0.19072E+00   0.30115E+00 0.23422E+01 
c  Velocity[X]                                      0.72613E-01 
c  Velocity[Y]                                      0.11955E+00 
c  Velocity[Z]                                      0.10899E+00 
c  Pressure     0.37054E-01     722   0.21927E-01   0.50924E-01 0.61607E-01 
c  k            0.26716E-01     160   0.23452E-03   0.34390E-04 0.24965E+01 
c  epsilon      0.23374E+03     114   0.50467E-03   0.44579E+04 0.10997E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0002313                            27
a  epsilon                -0.62989                            33
a  Local Time Step      4.2278e-08                        281665


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6198          4.9744         0.49914         0.11532
v  Velocity[Y]             -4.6239          6.8008         0.37848         0.27161
v  Velocity[Z]             -7.4328          4.5394          -0.293      -0.0015629
v  ǁVelocityǁ            0.0037542          8.3892          1.7951          2.2426
v  Pressure                -1956.3           26939           17987           14588
v  k                    1.1198e-08         0.73111       0.0085356        0.012323
v  epsilon               1.611e-05           23340          41.004          7.3619
v  TurbVisc             4.0934e-14         0.16883      0.00066191       0.0087626
v  CourantNb              0.034708           72215          106.42          24.613
v  FourierNb               0.22272      2.3653e+06          217.52           2.797
v  total_pressure       4.9804e+05      5.2694e+05      5.1799e+05      5.1459e+05
v  Local Time Step            0.01        0.060587        0.010002        0.010014


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set me   Friction velocity        uet   :  0.26553E-01 0.19541E+02
   Friction velocity        uk    :  0.26481E-01 0.19541E+02
   Dimensionless distance   yplus :  0.24935E-02 0.10390E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3867
   Nb of faces within the viscous sub-layer     :      24576
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67961E+00     424   0.19116E+00      Friction velocity        uet   :  0.26553E-01 0.19541E+02
   Friction velocity        uk    :  0.26481E-01 0.19541E+02
   Dimensionless distance   yplus :  0.24935E-02 0.10390E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3867
   Nb of faces within the viscous sub-layer     :      24576
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67961E+00     424   0.19116E+00   0   Friction velocity        uet   :  0.26553E-01 0.19541E+02
   Friction velocity        uk    :  0.26481E-01 0.19541E+02
   Dimensionless distance   yplus :  0.24935E-02 0.10390E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3867
   Nb of faces within the viscous sub-layer     :      24576
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67961E+00     424   0.19116E+00   0.30907E+00 0.23715E+01 
c  Velocity[X]                                      0.74926E-01 
c  Velocity[Y]                                      0.12889E+00 
c  Velocity[Z]                                      0.10525E+00 
c  Pressure     0.36849E-01     937   0.21156E-01   0.50480E-01 0.61982E-01 
c  k            0.26704E-01     140   0.22982E-03   0.32919E-04 0.24413E+01 
c  epsilon      0.23038E+03     104   0.38533E-03   0.49644E+04 0.11640E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00016468                            14
a  epsilon                 -26.291                            26
a  Local Time Step      4.2278e-08                        281658


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5833          4.9723         0.49949         0.11534
v  Velocity[Y]             -4.6346          6.7715         0.37818         0.27178
v  Velocity[Z]             -7.3353          4.4345        -0.29345      -0.0015026
v  ǁVelocityǁ            0.0034669          8.3877           1.796           2.243
v  Pressure                -1995.9           26938           17979           14582
v  k                    1.2463e-08         0.73355       0.0085804        0.012335
v  epsilon              6.4012e-06           23499          41.144          7.3737
v  TurbVisc             9.4058e-14         0.16883      0.00066694       0.0087651
v  CourantNb              0.040351           74450          106.43          24.621
v  FourierNb               0.22278      2.3653e+06          217.53          2.7972
v  total_pressure         4.98e+05      5.2694e+05      5.1798e+05      5.1458e+05
v  Local Time Step            0.01        0.066645        0.010002        0.010016


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6713      2.3807e+06          323.96          27.418


 TIME FOR THE TIME STEP              229:        0.15528E+03

===============================================================


 INSTANT    0.230000000E+02   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        -0.150663318E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441825E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25049E+01 0.19035E+01
   Friction velocity        uet   :  0.18089E-01 0.19725E+02
   Friction velocity        uk    :  0.18003E-01 0.19725E+02
   Dimensionless distance   yplus :  0.25170E-02 0.10361E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3867
   Nb of faces within the viscous sub-layer     :      24555
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68013E+00     425   0.19249E+00   0.30156E+00 0.23425E+01 
c  Velocity[X]                                      0.70875E-01 
c  Velocity[Y]                                      0.12705E+00 
c  Velocity[Z]                                      0.10363E+00 
c  Pressure     0.36245E-01    1061   0.20501E-01   0.49512E-01 0.10221E+00 
c  k            0.26765E-01     133   0.25197E-03   0.36517E-04 0.25702E+01 
c  epsilon      0.23786E+03     110   0.39214E-03   0.41119E+04 0.10509E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.5796e-05                      TIME FOR THE TIME STEP              230:        0.15653E+03

===============================================================


 INSTANT    0.231000000E+02   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        -0.989743724E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441850E+0 TIME FOR THE TIME STEP              230:        0.16132E+03

===============================================================


 INSTANT    0.231000000E+02   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        -0.989743724E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441850E+00 TIME FOR THE TIME STEP              230:        0.15912E+03

===============================================================


 INSTANT    0.231000000E+02   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        -0.989743724E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441850E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25007E+01 0.19052E+01
   Friction velocity        uet   :  0.18686E-01 0.19276E+02
   Friction velocity        uk    :  0.18593E-01 0.19276E+02
   Dimensionless distance   yplus :  0.23311E-02 0.10330E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3875
   Nb of faces within the viscous sub-layer     :      24532
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68001E+00     425   0.18997E+00   0.30841E+00 0.23688E+01 
c  Velocity[X]                                      0.73801E-01 
c  Velocity[Y]                                      0.13158E+00 
c  Velocity[Z]                                      0.10302E+00 
c  Pressure     0.36176E-01    1084   0.19868E-01   0.49324E-01 0.12921E+00 
c  k            0.26751E-01     143   0.22609E-03   0.37660E-04 0.26091E+01 
c  epsilon      0.23300E+03     114   0.32866E-03   0.35129E+04 0.97690E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00016635                            12
a  epsilon                 -26.569                            17
a  Local Time Step      4.2278e-08                        281664


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5688          5.0002          0.5013         0.11514
v  Velocity[Y]              -4.629           6.782         0.37756         0.27192
v  Velocity[Z]             -7.5053          4.4177        -0.29426      -0.0015504
v  ǁVelocityǁ            0.0031746          8.5626          1.7981          2.2433
v  Pressure                -2061.2           26897           17931           14550
v  k                    1.3738e-08         0.73895       0.0086429        0.012354
v  epsilon              0.00010848           23812          41.272          7.4105
v  TurbVisc             6.2506e-14         0.16883      0.00067551       0.0087685
v  CourantNb             0.0055626           79685          106.36          24.633
v  FourierNb               0.22287      2.3653e+06          217.54          2.7988
v  total_pressure       4.9794e+05       5.269e+05      5.1793e+05      5.1455e+05
v  Local Time Step            0.01        0.080641        0.010003        0.010019


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6857      2.3792e+06          323.89          27.432


 TIME FOR THE TIME STEP              231:        0.16393E+03

===============================================================


 INSTANT    0.232000000E+02   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        -0.117909048E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441844E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24917E+01 0.19103E+01
   Friction velocity        uet   :  0.12719E-01 0.19650E+02
   Friction velocity        uk    :  0.12634E-01 0.19650E+02
   Dimensionless distance   yplus :  0.25074E-02 0.10408E+0
   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5138          4.9829         0.50214         0.11493
v  Velocity[Y]              -4.617          6.7885         0.37648         0.27193
v  Velocity[Z]             -7.5658          4.6181        -0.29485      -0.0015655
v  ǁVelocityǁ            0.0043104          8.6373          1.7987          2.2434
v  Pressure                  -2087           26860           17892           14523
v  k                    1.3984e-08         0.73697       0.0086706        0.012357
v  epsilon              0.00013967           23716          41.493          7.4207
v  TurbVisc             9.6828e-14         0.16883      0.00067787       0.0087701
v  Cour
   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5138          4.9829         0.50214         0.11493
v  Velocity[Y]              -4.617          6.7885         0.37648         0.27193
v  Velocity[Z]             -7.5658          4.6181        -0.29485      -0.0015655
v  ǁVelocityǁ            0.0043104          8.6373          1.7987          2.2434
v  Pressure                  -2087           26860           17892           14523
v  k                    1.3984e-08         0.73697       0.0086706        0.012357
v  epsilon              0.00013967           23716          41.493          7.4207
v  TurbVisc             9.6828e-14         0.16883      0.00067787       0.0087701
v  Coura
   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5138          4.9829         0.50214         0.11493
v  Velocity[Y]              -4.617          6.7885         0.37648         0.27193
v  Velocity[Z]             -7.5658          4.6181        -0.29485      -0.0015655
v  ǁVelocityǁ            0.0043104          8.6373          1.7987          2.2434
v  Pressure                  -2087           26860           17892           14523
v  k                    1.3984e-08         0.73697       0.0086706        0.012357
v  epsilon              0.00013967           23716          41.493          7.4207
v  TurbVisc             9.6828e-14         0.16883      0.00067787       0.0087701
v  CourantNb              0.076527           79972          106.28          24.635
v  FourierNb               0.22289      2.3653e+06          217.54          2.7988
v  total_pressure       4.9791e+05      5.2686e+05      5.1789e+05      5.1452e+05
v  Local Time Step            0.01        0.088705        0.010003        0.010022


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5821      2.3776e+06          323.81          27.434


 TIME FOR THE TIME STEP              232:        0.16386E+03

===============================================================


 INSTANT    0.233000000E+02   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        -0.473485555E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441858E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24738E+01 0.19059E+01
   Friction velocity        uet   :  0.16162E-01 0.21229E+02
   Friction velocity        uk    :  0.16123E-01 0.21229E+02
   Dimensionless distance   yplus :  0.27088E-02 0.10366E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3864
   Nb of faces within the viscous sub-layer     :      24513
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67980E+00     419   0.19301E+00   0.30473E+00 0.23542E+01 
c  Velocity[X]                                      0.79123E-01 
c  Velocity[Y]                                      0.12349E+00 
c  Velocity[Z]                                      0.10211E+00 
c  Pressure     0.35245E-01    1123   0.19039E-01   0.47990E-01 0.18078E+00 
c  k            0.26724E-01     134   0.23615E-03   0.35015E-04 0.25151E+01 
c  epsilon      0.23049E+03     104   0.33247E-03   0.38596E+04 0.10265E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011839                            20
a  epsilon                 -27.129                            26
a  Local Time Step      4.2278e-08                        281651


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5768           4.966         0.50229         0.11471
v  Velocity[Y]              -4.617           6.704         0.37609         0.27212
v  Velocity[Z]             -7.6237          4.3967        -0.29586      -0.0014145
v  ǁVelocityǁ            0.0040735          8.7184          1.7995          2.2434
v  Pressure                -2087.4           26822           17853           14497
v  k                    1.5491e-08          0.7375       0.0086484        0.012358
v  epsilon              8.7512e-05           23745            41.2          7.4143
v  TurbVisc             9.2202e-14         0.16883       0.0006791       0.0087703
v  CourantNb               0.02993           78863           106.1          24.638
v  FourierNb               0.22287      2.3653e+06          217.54          2.7993
v  total_pressure       4.9791e+05      5.2682e+05      5.1785e+05       5.145e+05
v  Local Time Step            0.01        0.097575        0.010003        0.010024


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5375      2.3722e+06          323.64          27.437


 TIME FOR THE TIME STEP              233:        0.16155E+03

===============================================================


 INSTANT    0.234000000E+02   TIME STEP NUMBER     Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67956E+00     416   0.19193E+00   0.30388E+00 0.23507E+01 
c  Velocity[X]                                      0.76984E-01 
c  Velocity[Y]                                      0.12266E+00 
c  Velocity[Z]                                      0.10423E+00 
c  Pressure     0.36295E-01    1064   0.19198E-01   0.49358E-01 0.12612E+00 
c  k            0.26716E-01     155   0.24842E-03   0.32932E-04 0.   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67956E+00     416   0.19193E+00   0.30388E+00 0.23507E+01 
c  Velocity[X]                                      0.76984E-01 
c  Velocity[Y]                                      0.12266E+00 
c  Velocity[Z]                                      0.10423E+00 
c  Pressure     0.36295E-01    1064   0.19198E-01   0.49358E-01 0.12612E+00 
c  k            0.26716E-01     155   0.24842E-03   0.32932E-04 0.2   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67956E+00     416   0.19193E+00   0.30388E+00 0.23507E+01 
c  Velocity[X]                                      0.76984E-01 
c  Velocity[Y]                                      0.12266E+00 
c  Velocity[Z]                                      0.10423E+00 
c  Pressure     0.36295E-01    1064   0.19198E-01   0.49358E-01 0.12612E+00 
c  k            0.26716E-01     155   0.24842E-03   0.32932E-04 0.24386E+01 
c  epsilon      0.22713E+03     106   0.54982E-03   0.48028E+04 0.11409E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.3687e-05                            10
a  epsilon                -0.05312                            12
a  Local Time Step      4.2278e-08                        281663


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5632          4.9587         0.50262         0.11435
v  Velocity[Y]             -4.6188           6.658         0.37506         0.27227
v  Velocity[Z]             -7.6337          4.6365         -0.2975      -0.0014047
v  ǁVelocityǁ            0.0022848          8.7508          1.8003          2.2434
v  Pressure                -2066.1           26798           17829           14480
v  k                    1.6737e-08         0.73524       0.0086808         0.01236
v  epsilon              0.00013132           23642          41.488          7.4258
v  TurbVisc             1.0739e-13         0.16883      0.00068066       0.0087707
v  CourantNb              0.035761           78859          106.01          24.641
v  FourierNb               0.22285      2.3653e+06          217.54          2.7993
v  total_pressure       4.9793e+05       5.268e+05      5.1783e+05      5.1448e+05
v  Local Time Step            0.01         0.10733        0.010003        0.010026


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5538      2.3716e+06          323.55          27.441


 TIME FOR THE TIME STEP              234:        0.15789E+03

===============================================================


 INSTANT    0.235000000E+02   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        -0.104462660E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441803E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24670E+01 0.19086E+01
   Friction velocity        uet   :  0.89135E-02 0.21734E+02
   Friction velocity        uk    :  0.88686E-02 0.21734E+02
   Dimensionless distance   yplus :  0.27733E-02 0.10361E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3866
   Nb of faces within the viscous sub-layer     :      24504
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68037E+00     419   0.19472E+00   0.30113E+00 0.23401E+01 
c  Velocity[X]                                      0.79887E-01 
c  Velocity[Y]                                      0.11585E+00 
c  Velocity[Z]                                      0.10539E+00 
c  Pressure     0.35396E-01    1084   0.18772E-01   0.48108E-01 0.14017E+00 
c  k            0.26720E-01     150   0.20145E-03   0.31290E-04 0.23773E+01 
c  epsilon      0.23050E+03     110   0.32359E-03   0.47138E+04 0.11343E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.3317e-05                            11
a  epsilon                -0.91511                            19
a  Local Time Step      4.2278e-08                        281661


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  ---------------------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.106699143E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441860E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUN---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.106699143E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441860E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUND---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.106699143E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441860E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24713E+01 0.19122E+01
   Friction velocity        uet   :  0.16215E-01 0.19548E+02
   Friction velocity        uk    :  0.16015E-01 0.19548E+02
   Dimensionless distance   yplus :  0.24943E-02 0.10323E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3857
   Nb of faces within the viscous sub-layer     :      24505
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67956E+00     411   0.19657E+00   0.29669E+00 0.23227E+01 
c  Velocity[X]                                      0.82947E-01 
c  Velocity[Y]                                      0.11664E+00 
c  Velocity[Z]                                      0.97101E-01 
c  Pressure     0.35105E-01    1080   0.18664E-01   0.47690E-01 0.13473E+00 
c  k            0.26706E-01     140   0.20377E-03   0.32122E-04 0.24086E+01 
c  epsilon      0.22805E+03     109   0.31522E-03   0.28290E+04 0.87869E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00013581                            12
a  epsilon                 -21.438                            19
a  Local Time Step      4.2278e-08                        281653


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5081          4.9597         0.50305         0.11423
v  Velocity[Y]             -4.6014          6.6767         0.37254         0.27244
v  Velocity[Z]             -7.6263          4.5877        -0.29779      -0.0013182
v  ǁVelocityǁ            0.0025613          8.7693          1.7998          2.2431
v  Pressure                -2026.8           26746           17781           14443
v  k                    1.8101e-08         0.73723       0.0086709        0.012359
v  epsilon              4.9524e-05           23730          41.052          7.4177
v  TurbVisc             1.1569e-13         0.16883        0.000684       0.0087714
v  CourantNb              0.075157           79352          105.92          24.636
v  FourierNb               0.22279      2.3653e+06          217.55          2.8001
v  total_pressure       4.9797e+05      5.2675e+05      5.1778e+05      5.1444e+05
v  Local Time Step            0.01         0.12987        0.010004        0.010033


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6217      2.3751e+06          323.47          27.436


 TIME FOR THE TIME STEP              236:        0.15624E+03

===============================================================


 INSTANT    0.237000000E+02   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        -0.408494379E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441841E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24837E+01 0.19039E+01
   Friction velocity        uet   :  0.19928E-01 0.19081E+02
   Friction velocity        uk    :  0.19808E-01 0.19081E+02
   Dimensionless distance   yplus :  0.24348E-02 0.10287E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3872
   Nb of faces within the viscous sub-layer     :      24504
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVEv  Velocity[Z]             -7.6612          4.3659         -0.2986      -0.0013283
v  ǁVelocityǁ            0.0039761          8.8078          1.8002          2.2428
v  Pressure                -2030.2           26723           17762           14428
v  k                     1.799e-08         0.73428       0.0086879        0.012363
v  epsilon                1.72e-05           23640          41.148          7.4199
v  TurbVisc             1.2117e-13         0.16883      0.00068438       0.0087719
v  CourantNb               0.10273           76857          105.81          24.635
v  FourierNb               0.22277      2.3653e+06          217.55          2.8006
v  total_pressure       4.9797e+05      5.2672e+05      5.1776e+05      5.1443e+05
v  Local Time Step            0.01         0.14286        0.010004        0.010035


  ** Cv  Velocity[Z]             -7.6612          4.3659         -0.2986      -0.0013283
v  ǁVelocityǁ            0.0039761          8.8078          1.8002          2.2428
v  Pressure                -2030.2           26723           17762           14428
v  k                     1.799e-08         0.73428       0.0086879        0.012363
v  epsilon                1.72e-05           23640          41.148          7.4199
v  TurbVisc             1.2117e-13         0.16883      0.00068438       0.0087719
v  CourantNb               0.10273           76857          105.81          24.635
v  FourierNb               0.22277      2.3653e+06          217.55          2.8006
v  total_pressure       4.9797e+05      5.2672e+05      5.1776e+05      5.1443e+05
v  Local Time Step            0.01         0.14286        0.010004        0.010035


  ** Cov  Velocity[Z]             -7.6612          4.3659         -0.2986      -0.0013283
v  ǁVelocityǁ            0.0039761          8.8078          1.8002          2.2428
v  Pressure                -2030.2           26723           17762           14428
v  k                     1.799e-08         0.73428       0.0086879        0.012363
v  epsilon                1.72e-05           23640          41.148          7.4199
v  TurbVisc             1.2117e-13         0.16883      0.00068438       0.0087719
v  CourantNb               0.10273           76857          105.81          24.635
v  FourierNb               0.22277      2.3653e+06          217.55          2.8006
v  total_pressure       4.9797e+05      5.2672e+05      5.1776e+05      5.1443e+05
v  Local Time Step            0.01         0.14286        0.010004        0.010035


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6407       2.372e+06          323.35          27.435


 TIME FOR THE TIME STEP              237:        0.15481E+03

===============================================================


 INSTANT    0.238000000E+02   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        -0.167852130E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441852E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24792E+01 0.19121E+01
   Friction velocity        uet   :  0.21915E-01 0.17695E+02
   Friction velocity        uk    :  0.21780E-01 0.17695E+02
   Dimensionless distance   yplus :  0.22579E-02 0.10312E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3869
   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     0.67985E+00     409   0.19405E+00   0.26096E+00 0.21781E+01 
c  Velocity[X]                                      0.74287E-01 
c  Velocity[Y]                                      0.10070E+00 
c  Velocity[Z]                                      0.85966E-01 
c  Pressure     0.33333E-01    1050   0.17550E-01   0.45266E-01 0.12307E+00 
c  k            0.26695E-01     128   0.18974E-03   0.22562E-04 0.20187E+01 
c  epsilon      0.22785E+03     108   0.16900E-03   0.12249E+04 0.57928E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00027414                            16
a  epsilon                 -1.1371                            17
a  Local Time Step      4.2278e-08                        281643


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5232          4.9859         0.50438         0.11432
v  Velocity[Y]             -4.5998          6.5968           0.373         0.27225
v  Velocity[Z]             -7.6356          4.4006        -0.29834      -0.0015298
v  ǁVelocityǁ            0.0039911          8.7649          1.8004          2.2427
v  Pressure                -2041.3           26700           17742           14411
v  k                    1.7217e-08         0.73802       0.0086869        0.012363
v  epsilon              5.8213e-05           23785          41.136          7.4113
v  TurbVisc             1.1766e-13         0.16883      0.00068485       0.0087727
v  CourantNb              0.071226           77008           105.9          24.628
v  FourierNb                0.2228      2.3653e+06          217.55          2.8004
v  total_pressure       4.9796e+05       5.267e+05      5.1774e+05      5.1441e+05
v  Local Time Step            0.01         0.15715        0.010005        0.010038


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6731      2.3762e+06          323.44          27.429


 TIME FOR THE TIME STEP              238:        0.15573E+03

===============================================================


 INSTANT    0.239000000E+02   TIME STEP NUMBER             239
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
I-----------------------------------------------------------------------------
c  Velocity     0.67985E+00     406   0.19655E+00   0.25470E+00 0.21517E+01 
c  Velocity[X]                                      0.70326E-01 
c  Velocity[Y]                                      0.96452E-01 
c  Velocity[Z]                                      0.87921E-01 
c  Pressure     0.33000E-01    1117   0.16834E-01   0.44817E-01 0.15555E+00 
c  k            0.26697E-01     132   0.19407E-03   0.26742E-04 0.21975E+01 
c  epsilon      0.22911E+03     105   0.20684E-03   0.14948E+04 0.64193E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  ---------------------------------------------------------------------------------
c  Velocity     0.67985E+00     406   0.19655E+00   0.25470E+00 0.21517E+01 
c  Velocity[X]                                      0.70326E-01 
c  Velocity[Y]                                      0.96452E-01 
c  Velocity[Z]                                      0.87921E-01 
c  Pressure     0.33000E-01    1117   0.16834E-01   0.44817E-01 0.15555E+00 
c  k            0.26697E-01     132   0.19407E-03   0.26742E-04 0.21975E+01 
c  epsilon      0.22911E+03     105   0.20684E-03   0.14948E+04 0.64193E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  ----------------------------------------------------------------------------------
c  Velocity     0.67985E+00     406   0.19655E+00   0.25470E+00 0.21517E+01 
c  Velocity[X]                                      0.70326E-01 
c  Velocity[Y]                                      0.96452E-01 
c  Velocity[Z]                                      0.87921E-01 
c  Pressure     0.33000E-01    1117   0.16834E-01   0.44817E-01 0.15555E+00 
c  k            0.26697E-01     132   0.19407E-03   0.26742E-04 0.21975E+01 
c  epsilon      0.22911E+03     105   0.20684E-03   0.14948E+04 0.64193E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00014161                            10
a  epsilon                 -1.0297                            15
a  Local Time Step      4.2278e-08                        281646


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5759          4.9978         0.50444         0.11446
v  Velocity[Y]             -4.5999          6.5901         0.37337         0.27208
v  Velocity[Z]             -7.6746           4.362        -0.29799      -0.0016477
v  ǁVelocityǁ            0.0053251          8.7688          1.7999          2.2424
v  Pressure                  -2063           26669           17712           14388
v  k                     1.731e-08         0.73472       0.0086825        0.012368
v  epsilon              4.2012e-05           23650          40.855          7.4136
v  TurbVisc             1.1314e-13         0.16883      0.00068568       0.0087738
v  CourantNb             0.0088889           74775           105.9          24.626
v  FourierNb               0.22282      2.3653e+06          217.55          2.8007
v  total_pressure       4.9794e+05      5.2667e+05      5.1771e+05      5.1439e+05
v  Local Time Step            0.01         0.16613        0.010005        0.010041


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6445      2.3732e+06          323.45          27.426


 TIME FOR THE TIME STEP              239:        0.15947E+03

===============================================================


 INSTANT    0.240000000E+02   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        -0.113782370E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441827E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25128E+01 0.19088E+01
   Friction velocity        uet   :  0.13078E-01 0.15697E+02
   Friction velocity        uk    :  0.12979E-01 0.15697E+02
   Dimensionless distance   yplus :  0.20030E-02 0.10169E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3863
   Nb of faces within the viscous sub-layer     :      24511
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67920E+00     405   0.19618E+00   0.25595E+00 0.21565E+01 
c  Velocity[X]                                      0.71481E-01 
c  Velocity[Y]                                      0.95180E-01 
c  Velocity[Z]                                      0.89291E-01 
c  Pressure     0.31264E-01    1063   0.15513E-01   0.42409E-01 0.11362E+00 
c  k            0.26692E-01     136   0.21872E-03   0.27866E-04 0.22433E+01 
c  epsilon      0.22660E+03     105   0.31970E-03   0.31801E+04 0.93387E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00025365                            11
a  epsilon                 -1.0633                            13
a  Local Time Step      4.2278e-08                        281640


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5538          5.0328         0.50487         0.11449
v  Velocity[Y]             -4.6292           6.511         0.37243         0.27215
v  Velocity[Z]             -7.6658          4.3736        -0.29735      -0.0017316
v  ǁVelocityǁ            0.0041739          8.7427          1.7991          2.2425
v  PressureSymmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441851E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25316E+01 0.19097E+01
   Friction velocity        uet   :  0.21605E-01 0.16250E+02Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441851E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25316E+01 0.19097E+01
   Friction velocity        uet   :  0.21605E-01 0.16250E+02
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441851E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25316E+01 0.19097E+01
   Friction velocity        uet   :  0.21605E-01 0.16250E+02
   Friction velocity        uk    :  0.21471E-01 0.16250E+02
   Dimensionless distance   yplus :  0.20735E-02 0.10249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3868
   Nb of faces within the viscous sub-layer     :      24508
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68003E+00     406   0.19284E+00   0.25346E+00 0.21457E+01 
c  Velocity[X]                                      0.68044E-01 
c  Velocity[Y]                                      0.97038E-01 
c  Velocity[Z]                                      0.88381E-01 
c  Pressure     0.29678E-01     974   0.14345E-01   0.40243E-01 0.65555E-01 
c  k            0.26687E-01     136   0.21504E-03   0.27152E-04 0.22143E+01 
c  epsilon      0.22805E+03     112   0.34395E-03   0.28769E+04 0.89125E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00050567                            17
a  epsilon                 -4.4445                            18
a  Local Time Step      4.2278e-08                        281642


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -2.546          5.0148         0.50437         0.11472
v  Velocity[Y]             -4.6397          6.5921         0.37254         0.27219
v  Velocity[Z]              -7.695          4.3461        -0.29718      -0.0016668
v  ǁVelocityǁ             0.002268          8.7529          1.7997          2.2426
v  Pressure                -2094.2           26638           17678           14364
v  k                    1.1898e-08         0.73886       0.0086885         0.01237
v  epsilon              0.00012186           23857          41.002          7.4092
v  TurbVisc             1.1652e-13         0.16883       0.0006877       0.0087757
v  CourantNb               0.11206           75069          105.76          24.617
v  FourierNb               0.22295      2.3653e+06          217.55          2.8013
v  total_pressure       4.9791e+05      5.2664e+05      5.1768e+05      5.1436e+05
v  Local Time Step            0.01         0.11039        0.010005        0.010044


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6413      2.3731e+06          323.31          27.418


 TIME FOR THE TIME STEP              241:        0.15021E+03

===============================================================


 INSTANT    0.242000000E+02   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        -0.628765995E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441831E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25278E+01 0.19093E+01
   Friction velocity        uet   :  0.18492E-01 0.16193E+02
   Friction velocity        uk    :  0.18249E-01 0.16193E+02
   Dimensionless distance   yplus :  0.20662E-02 0.10101E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3875
   Nb of faces within the viscous sub-layer     :      24497
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68042E+00     394   0.19852E+00   0.24901Ev  epsilon              6.1813e-05           23606          41.011          7.4144
v  TurbVisc             7.4321e-14         0.16883      0.00068774       0.0087766
v  CourantNb              0.015043           74510          105.79          24.618
v  FourierNb               0.22302      2.3653e+06          217.55           2.801
v  total_pressure        4.979e+05      5.2663e+05      5.1767e+05      5.1436e+05
v  Local Time Step            0.01         0.11239        0.010005        0.010044


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6369      2.3758e+06          323.34          27.419


 TIME FOR THE TIME STEP     v  epsilon              6.1813e-05           23606          41.011          7.4144
v  TurbVisc             7.4321e-14         0.16883      0.00068774       0.0087766
v  CourantNb              0.015043           74510          105.79          24.618
v  FourierNb               0.22302      2.3653e+06          217.55           2.801
v  total_pressure        4.979e+05      5.2663e+05      5.1767e+05      5.1436e+05
v  Local Time Step            0.01         0.11239        0.010005        0.010044


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6369      2.3758e+06          323.34          27.419


 TIME FOR THE TIME STEP      v  epsilon              6.1813e-05           23606          41.011          7.4144
v  TurbVisc             7.4321e-14         0.16883      0.00068774       0.0087766
v  CourantNb              0.015043           74510          105.79          24.618
v  FourierNb               0.22302      2.3653e+06          217.55           2.801
v  total_pressure        4.979e+05      5.2663e+05      5.1767e+05      5.1436e+05
v  Local Time Step            0.01         0.11239        0.010005        0.010044


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6369      2.3758e+06          323.34          27.419


 TIME FOR THE TIME STEP              242:        0.14687E+03

===============================================================


 INSTANT    0.243000000E+02   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        -0.715646353E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441820E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25262E+01 0.19041E+01
   Friction velocity        uet   :  0.25417E-01 0.16893E+02
   Friction velocity        uk    :  0.25130E-01 0.16893E+02
   Dimensionless distance   yplus :  0.21556E-02 0.10121E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3885
   Nb of faces within the viscous sub-layer     :      24502
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67991E+00     389   0.19412E+00   0.25549E+00 0.21549E+01 
c  Velocity[X]                                      0.71933E-01 
c  Velocity[Y]                                      0.96466E-01 
c  Velocity[Z]                                      0.87089E-01 
c  Pressure     0.29414E-01     665   0.14069E-01   0.39810E-01 0.28552E-01 
c  k            0.26738E-01     132   0.33132E-03   0.26982E-04 0.22064E+01 
c  epsilon      0.23090E+03     105   0.49844E-03   0.38993E+04 0.10324E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00060065                            13
a  epsilon                 -1.2644                            16
a  Local Time Step      4.2278e-08                        281642


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5349          4.9839         0.50469         0.11489
v  Velocity[Y]             -4.6277          6.6456         0.37254         0.27226
v  Velocity[Z]             -7.7437          4.3638        -0.29614      -0.0015608
v  ǁVelocityǁ            0.0018076          8.7759          1.7999           2.242
v  Pressure                -2080.1           26634           17674           14359
v  k                    1.6214e-08         0.73457       0.0087366        0.012375
v  epsilon              1.1038e-05           23643           41.15          7.4354
v  TurbVisc             1.0484e-13         0.16883      0.00068882       0.0087773
v  CourantNb               0.11054           72743          105.83          24.621
v  FourierNb               0.22309      2.3653e+06          217.55          2.8013
v  total_pressure       4.9792e+05      5.2663e+05      5.1767e+05      5.1436e+05
v  Local Time Step            0.01         0.11253        0.010005        0.010045


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6304      2.3744e+06          323.39          27.422


 TIME FOR THE TIME STEP              243:        0.13726E+03

===============================================================


 INSTANT    0.244000000E+02   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        -0.135516193E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3   c  Velocity[Z]                                      0.82280E-01 
c  Pressure     0.28732E-01     775   0.13837E-01   0.38862E-01 0.31087E-01 
c  k            0.26715E-01     126   0.23148E-03   0.21509E-04 0.19707E+01 
c  epsilon      0.22826E+03     100   0.30675E-03   0.20986E+04 0.75950E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0006827                            26
a  epsilon                  -25.38                            33
a  Local Time Step      4.2278e-08                        281643


  ** Computed fields on cells
   c  Velocity[Z]                                      0.82280E-01 
c  Pressure     0.28732E-01     775   0.13837E-01   0.38862E-01 0.31087E-01 
c  k            0.26715E-01     126   0.23148E-03   0.21509E-04 0.19707E+01 
c  epsilon      0.22826E+03     100   0.30675E-03   0.20986E+04 0.75950E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0006827                            26
a  epsilon                  -25.38                            33
a  Local Time Step      4.2278e-08                        281643


  ** Computed fields on cells
    c  Velocity[Z]                                      0.82280E-01 
c  Pressure     0.28732E-01     775   0.13837E-01   0.38862E-01 0.31087E-01 
c  k            0.26715E-01     126   0.23148E-03   0.21509E-04 0.19707E+01 
c  epsilon      0.22826E+03     100   0.30675E-03   0.20986E+04 0.75950E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0006827                            26
a  epsilon                  -25.38                            33
a  Local Time Step      4.2278e-08                        281643


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5348          5.0173         0.50455         0.11496
v  Velocity[Y]             -4.6292          6.7136         0.37114         0.27233
v  Velocity[Z]             -7.6952          4.3957        -0.29526      -0.0016014
v  ǁVelocityǁ            0.0045286          8.7116          1.7995          2.2421
v  Pressure                -2084.2           26637           17676           14361
v  k                    1.7254e-08         0.73405       0.0086926        0.012369
v  epsilon              5.0832e-05           23617           40.83          7.4146
v  TurbVisc             1.0478e-13         0.16883      0.00069099       0.0087777
v  CourantNb              0.030083           71080          105.81          24.615
v  FourierNb               0.22313      2.3653e+06          217.56          2.8016
v  total_pressure       4.9792e+05      5.2664e+05      5.1768e+05      5.1436e+05
v  Local Time Step            0.01         0.11251        0.010005        0.010047


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.603      2.3779e+06          323.37          27.417


 TIME FOR THE TIME STEP              244:        0.14302E+03

===============================================================


 INSTANT    0.245000000E+02   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        -0.769652965E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441253E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24711E+01 0.19020E+01
   Friction velocity        uet   :  0.21381E-01 0.18764E+02
   Friction velocity        uk    :  0.21375E-01 0.18764E+02
   Dimensionless distance   yplus :  0.13343E-02 0.10259E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3880
   Nb of faces within the viscous sub-layer     :      24502
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68115E+00     381   0.19310E+00   0.24423E+00 0.21070E+01 
c  Velocity[X]                                      0.67164E-01 
c  Velocity[Y]                                      0.91391E-01 
c  Velocity[Z]                                      0.85679E-01 
c  Pressure     0.28394E-01     976   0.13653E-01   0.38392E-01 0.67282E-01 
c  k            0.26735E-01     132   0.22500E-03   0.22712E-04 0.20247E+01 
c  epsilon      0.23149E+03     110   0.69979E-03   0.24992E+04 0.82757E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00043685                            11
a  epsilon                 -1.0119                            16
a  Local Time Step      4.2278e-08                        281645


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5577          4.9695         0.50382         0.11499
v  Velocity[Y]             -4.6174          6.7606         0.37164         0.27245
v  Velocity[Z]             -7.6239          4.3822        -0.29485      -0.0016286
v  ǁVelocityǁ            0.0022186          8.6436          1.7998           2.242
v  Pressure                -2085.5           26653           17689           14370
v  k                    1.7872e-08         0.73175       0.0087314        0.012374
v  epsilon              5.0722e-05           23531          41.002          7.4294
v  TurbVisc       Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24441E+01 0.19080E+01
   Friction velocity        uet   :  0.96151E-02 0.19299E+02
   Friction velocity        uk    :  0.95547E-02 0.19299E+02
   Dimensionless distance   yplus :  0.11217E-02 0.10110E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3874
   Nb of facesFree surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24441E+01 0.19080E+01
   Friction velocity        uet   :  0.96151E-02 0.19299E+02
   Friction velocity        uk    :  0.95547E-02 0.19299E+02
   Dimensionless distance   yplus :  0.11217E-02 0.10110E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3874
   Nb of faces Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24441E+01 0.19080E+01
   Friction velocity        uet   :  0.96151E-02 0.19299E+02
   Friction velocity        uk    :  0.95547E-02 0.19299E+02
   Dimensionless distance   yplus :  0.11217E-02 0.10110E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3874
   Nb of faces within the viscous sub-layer     :      24501
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68042E+00     386   0.19538E+00   0.25030E+00 0.21333E+01 
c  Velocity[X]                                      0.72975E-01 
c  Velocity[Y]                                      0.93810E-01 
c  Velocity[Z]                                      0.83514E-01 
c  Pressure     0.28105E-01     883   0.13446E-01   0.37986E-01 0.43325E-01 
c  k            0.26731E-01     127   0.21415E-03   0.22280E-04 0.20051E+01 
c  epsilon      0.22832E+03      97   0.43345E-03   0.25123E+04 0.83247E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00047162                            14
a  epsilon                 -24.345                            22
a  Local Time Step      4.2278e-08                        281652


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6081           4.975         0.50458         0.11497
v  Velocity[Y]               -4.61          6.8187          0.3719         0.27239
v  Velocity[Z]             -7.6255          4.4059        -0.29336      -0.0016848
v  ǁVelocityǁ            0.0039726          8.6527          1.7993          2.2419
v  Pressure                  -2090           26660           17695           14375
v  k                    1.7707e-08         0.73422       0.0087193        0.012373
v  epsilon              4.5624e-05           23642           40.78          7.4254
v  TurbVisc             1.1722e-13         0.16883       0.0006932       0.0087775
v  CourantNb              0.018895           70867          105.79          24.618
v  FourierNb                0.2232      2.3653e+06          217.56          2.8018
v  total_pressure       4.9791e+05      5.2666e+05       5.177e+05      5.1437e+05
v  Local Time Step            0.01         0.12314        0.010006        0.010049


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier            1.61      2.3796e+06          323.35          27.419


 TIME FOR THE TIME STEP              246:        0.14868E+03

===============================================================


 INSTANT    0.247000000E+02   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        -0.952473442E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441234E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24500E+01 0.19055E+01
   Friction velocity        uet   :  0.26773E-01 0.16567E+02
   Friction velocity        uk    :  0.26319E-01 0.16567E+02
   Dimensionless distance   yplus :  0.16896E-02 0.10264E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3876
   Nb of faces within the viscous sub-layer     :      24492
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68068E+00     384   0.19196E+00   0.24264E+00 0.21006E+01 
c  Velocity[X]                                      0.69201E-01 
c  Velocity[Y]                                      0.93051E-01 
c  Velocity[Z]                                      0.80391E-01 
c  Pressure     0.26982E-01     862  v  FourierNb               0.22319      2.3653e+06          217.56          2.8019
v  total_pressure       4.9789e+05      5.2666e+05      5.1769e+05      5.1437e+05
v  Local Time Step            0.01         0.13546        0.010006        0.010048


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6301      2.3746e+06          323.23          27.417


 TIME FOR THE TIME STEP              247:        0.14362E+03

===============================================================


 INSTANT    0.248000000E+02   TIME STEP NUMBER             248
 ============================================================= 




   ** BOUNDARY MASv  FourierNb               0.22319      2.3653e+06          217.56          2.8019
v  total_pressure       4.9789e+05      5.2666e+05      5.1769e+05      5.1437e+05
v  Local Time Step            0.01         0.13546        0.010006        0.010048


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6301      2.3746e+06          323.23          27.417


 TIME FOR THE TIME STEP              247:        0.14775E+03

===============================================================


 INSTANT    0.248000000E+02   TIME STEP NUMBER             248
 ============================================================= 




   ** BOUNDARY MASSv  FourierNb               0.22319      2.3653e+06          217.56          2.8019
v  total_pressure       4.9789e+05      5.2666e+05      5.1769e+05      5.1437e+05
v  Local Time Step            0.01         0.13546        0.010006        0.010048


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6301      2.3746e+06          323.23          27.417


 TIME FOR THE TIME STEP              247:        0.14338E+03

===============================================================


 INSTANT    0.248000000E+02   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        -0.130619811E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441823E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24558E+01 0.19089E+01
   Friction velocity        uet   :  0.23156E-01 0.16810E+02
   Friction velocity        uk    :  0.23129E-01 0.16810E+02
   Dimensionless distance   yplus :  0.11288E-02 0.10266E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3875
   Nb of faces within the viscous sub-layer     :      24494
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68033E+00     404   0.19268E+00   0.22821E+00 0.20368E+01 
c  Velocity[X]                                      0.61466E-01 
c  Velocity[Y]                                      0.87938E-01 
c  Velocity[Z]                                      0.78804E-01 
c  Pressure     0.26660E-01     957   0.12285E-01   0.36022E-01 0.62780E-01 
c  k            0.26719E-01     130   0.18826E-03   0.16130E-04 0.17061E+01 
c  epsilon      0.22799E+03      96   0.65067E-03   0.23338E+04 0.80135E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00043066                            17
a  epsilon                 -29.492                            25
a  Local Time Step      4.2278e-08                        281646


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5716          4.9555         0.50489         0.11485
v  Velocity[Y]             -4.5998            6.92         0.37221         0.27235
v  Velocity[Z]             -7.7016           4.424         -0.2935      -0.0017263
v  ǁVelocityǁ            0.0032085          8.7356          1.7997          2.2421
v  Pressure                -2123.1           26645           17680           14362
v  k                    1.6831e-08         0.73334        0.008734        0.012373
v  epsilon              3.2082e-05           23609          40.795          7.4235
v  TurbVisc             1.1186e-13         0.16883      0.00069467       0.0087776
v  CourantNb              0.048035           67330          105.58          24.613
v  FourierNb               0.22317      2.3653e+06          217.56          2.8018
v  total_pressure       4.9788e+05      5.2665e+05      5.1768e+05      5.1436e+05
v  Local Time Step            0.01           0.149        0.010005        0.010045


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6336      2.3781e+06          323.14          27.414


 TIME FOR THE TIME STEP              248:        0.15446E+03

===============================================================


 INSTANT    0.249000000E+02   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        -0.576167249E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441870E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
-----------------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00045928                            11
a  epsilon                 -0.8296                            16
a  Local Time Step      4.2278e-08                        281638


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5365          4.9522         0.50494         0.11493
v  Velocity[Y]     -----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00045928                            11
a  epsilon                 -0.8296                            16
a  Local Time Step      4.2278e-08                        281638


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5365          4.9522         0.50494         0.11493
v  Velocity[Y]      -----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00045928                            11
a  epsilon                 -0.8296                            16
a  Local Time Step      4.2278e-08                        281638


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5365          4.9522         0.50494         0.11493
v  Velocity[Y]             -4.5917          6.9671         0.37293         0.27235
v  Velocity[Z]             -7.7263          4.4002        -0.29322      -0.0016048
v  ǁVelocityǁ            0.0038045          8.7684          1.7993          2.2416
v  Pressure                -2132.8           26639           17674           14358
v  k                    1.7704e-08         0.73364       0.0087522        0.012374
v  epsilon              5.3903e-05           23629          40.869          7.4278
v  TurbVisc              1.059e-13         0.16883      0.00069564       0.0087771
v  CourantNb              0.043348           66775          105.67          24.614
v  FourierNb               0.22315      2.3653e+06          217.56          2.8016
v  total_pressure       4.9787e+05      5.2664e+05      5.1767e+05      5.1436e+05
v  Local Time Step            0.01         0.15764        0.010005        0.010044


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5979      2.3701e+06          323.23          27.416


 TIME FOR THE TIME STEP              249:        0.14526E+03

===============================================================


 INSTANT    0.250000000E+02   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        -0.104833582E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441872E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24700E+01 0.19048E+01
   Friction velocity        uet   :  0.18216E-01 0.14393E+02
   Friction velocity        uk    :  0.17979E-01 0.14393E+02
   Dimensionless distance   yplus :  0.18365E-02 0.10265E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3866
   Nb of faces within the viscous sub-layer     :      24489
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68045E+00     383   0.18819E+00   0.23138E+00 0.20511E+01 
c  Velocity[X]                                      0.64426E-01 
c  Velocity[Y]                                      0.89719E-01 
c  Velocity[Z]                                      0.77235E-01 
c  Pressure     0.25493E-01     905   0.11519E-01   0.34436E-01 0.39220E-01 
c  k            0.26710E-01     128   0.20219E-03   0.19177E-04 0.18605E+01 
c  epsilon      0.22773E+03     103   0.42946E-03   0.36709E+04 0.10065E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00040914                            18
a  epsilon                 -22.895                            33
a  Local Time Step      4.2278e-08                        281648


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5779          4.9489         0.50423         0.11487
v  Velocity[Y]             -4.5925          6.8756         0.37341         0.27226
v  Velocity[Z]             -7.7493           4.419        -0.29409       -0.001587
v  ǁVelocityǁ            0.0035418          8.8085          1.7992          2.2418
v  Pressure                  -2141           26631           17667           14353
v  k                    1.7671e-08         0.73129       0.0087529         0.01237
v  epsilon              3.8145e-05           23520          40.857          7.4213
v  TurbVisc             1.1456e-13         0.16883      0.00069607       0.0087766
v  CourantNb              0.038689           67527           105.6          24.608
v  FourierNb               0.22312      2.3653e+06          217.57          2.8019
v  total_pressure       4.9786e+05      5.2663e+0------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24806E+01 0.19036E+01
   Friction velocity        uet   :  0.21109E-01 0.15791E+02
   Friction velocity        uk    :  0.21093E-01 0.15791E+02
   Dimensionless distance   yplus :  0.20149E-02 0.10103E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3872
   Nb of faces within the viscous sub-layer     :      24500
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
------------------------------------------------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24806E+01 0.19036E+01
   Friction velocity        uet   :  0.21109E-01 0.15791E+02
   Friction velocity        uk    :  0.21093E-01 0.15791E+02
   Dimensionless distance   yplus :  0.20149E-02 0.10103E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3872
   Nb of faces within the viscous sub-layer     :      24500
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-------------------------------------------------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24806E+01 0.19036E+01
   Friction velocity        uet   :  0.21109E-01 0.15791E+02
   Friction velocity        uk    :  0.21093E-01 0.15791E+02
   Dimensionless distance   yplus :  0.20149E-02 0.10103E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3872
   Nb of faces within the viscous sub-layer     :      24500
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68086E+00     383   0.19168E+00   0.23144E+00 0.20514E+01 
c  Velocity[X]                                      0.66134E-01 
c  Velocity[Y]                                      0.89768E-01 
c  Velocity[Z]                                      0.75541E-01 
c  Pressure     0.25302E-01     870   0.11361E-01   0.34162E-01 0.35419E-01 
c  k            0.26729E-01     133   0.20081E-03   0.19348E-04 0.18686E+01 
c  epsilon      0.23150E+03     105   0.36845E-03   0.16777E+04 0.67871E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00044986                            11
a  epsilon                -0.73591                            18
a  Local Time Step      4.2278e-08                        281644


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5897          4.9591         0.50384          0.1149
v  Velocity[Y]             -4.5873          6.9278         0.37402         0.27228
v  Velocity[Z]             -7.7712          4.8481        -0.29567      -0.0016047
v  ǁVelocityǁ            0.0021068          8.8326          1.7998          2.2416
v  Pressure                -2147.7           26623           17660           14349
v  k                    1.7102e-08         0.73505       0.0087442         0.01237
v  epsilon              8.8241e-05           23697          40.843          7.4221
v  TurbVisc             1.1159e-13         0.16883      0.00069581       0.0087763
v  CourantNb              0.023492           64102          105.57          24.612
v  FourierNb               0.22309      2.3653e+06          217.56          2.8018
v  total_pressure       4.9785e+05      5.2662e+05      5.1766e+05      5.1435e+05
v  Local Time Step            0.01         0.15764        0.010006        0.010047


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.626      2.3729e+06          323.13          27.414


 TIME FOR THE TIME STEP              251:        0.14727E+03

===============================================================


 INSTANT    0.252000000E+02   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        -0.688244121E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441857E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24808E+01 0.19024E+01
   Friction velocity        uet   :  0.19953E-01 0.15494E+02
   Friction velocity        uk    :  0.19909E-01 0.15494E+02
   Dimensionless distance   yplus :  0.19770E-02 0.10256E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3865
   Nb of faces within the viscous sub-layer     :      24486
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67983E+00     379   0.19426E+00   0.23012E+00 0.20458E+01 
c  Velocity[X]                                      0.68122E-01 
c  Velocity[Y]                                      0.87942E-01 
c  Velocity[Z]                                      0.74054E-01 
c  Pressure     0.25667E-01     994   0.11628E-01   0.34619E-01 0.72349E-01 
c  k            0.26721E-01     127   0.23238E-03   0.18607E-04 0.18325E+01 
c  epsilon      0.22828E+03     100   0.42612E-03   0.20219E+04 0.74656E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fiel
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6368      2.3709e+06          323.16           27.41


 TIME FOR THE TIME STEP              252:        0.15137E+03

===============================================================


 INSTANT    0.253000000E+02   TIME STEP NUMBER             253
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Sm
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6368      2.3709e+06          323.16           27.41


 TIME FOR THE TIME STEP              252:        0.15457E+03

===============================================================


 INSTANT    0.253000000E+02   TIME STEP NUMBER             253
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smo
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6368      2.3709e+06          323.16           27.41


 TIME FOR THE TIME STEP              252:        0.15130E+03

===============================================================


 INSTANT    0.253000000E+02   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        -0.717303587E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441898E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24828E+01 0.19030E+01
   Friction velocity        uet   :  0.10300E-01 0.15348E+02
   Friction velocity        uk    :  0.10224E-01 0.15348E+02
   Dimensionless distance   yplus :  0.16729E-02 0.10252E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3873
   Nb of faces within the viscous sub-layer     :      24501
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68051E+00     374   0.19688E+00   0.23403E+00 0.20633E+01 
c  Velocity[X]                                      0.64722E-01 
c  Velocity[Y]                                      0.89598E-01 
c  Velocity[Z]                                      0.79709E-01 
c  Pressure     0.26477E-01     978   0.11846E-01   0.35700E-01 0.57935E-01 
c  k            0.26697E-01     130   0.21570E-03   0.21633E-04 0.19765E+01 
c  epsilon      0.23001E+03     106   0.38703E-03   0.28778E+04 0.89177E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00041383                            15
a  epsilon                 -1.8046                            25
a  Local Time Step      4.2278e-08                        281646


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5391          5.0092         0.50376         0.11508
v  Velocity[Y]             -4.5956           6.933         0.37476         0.27241
v  Velocity[Z]             -7.7655          4.4016        -0.29713      -0.0015791
v  ǁVelocityǁ            0.0025704          8.8541          1.8001          2.2414
v  Pressure                -2153.4           26593           17634           14330
v  k                     1.456e-08         0.73456       0.0087409        0.012367
v  epsilon              5.1043e-05           23692          40.801          7.4125
v  TurbVisc             1.0155e-13         0.16883      0.00069512       0.0087764
v  CourantNb              0.075615           62443          105.68          24.609
v  FourierNb               0.22305      2.3653e+06          217.56          2.8016
v  total_pressure       4.9785e+05      5.2659e+05      5.1763e+05      5.1433e+05
v  Local Time Step            0.01         0.15765        0.010005        0.010046


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6229      2.3748e+06          323.24          27.411


 TIME FOR THE TIME STEP              253:        0.14853E+03

===============================================================


 INSTANT    0.254000000E+02   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        -0.108956528E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441857E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
----------------------------------------------a  k                   -0.00042169                            14
a  epsilon                 -28.647                            23
a  Local Time Step      4.2278e-08                        281638


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5823          5.0002         0.50324         0.11508
v  Velocity[Y]             -4.6044          6.7283         0.37514          0.2724
v  Velocity[Z]             -7.7464          4.4231        -0.29766      -0.0016672
v  ǁVelocityǁ            0.0029685           8.821          1.8008          2.2415
v  Pressure                -2142.6           26587           17631           14328a  k                   -0.00042169                            14
a  epsilon                 -28.647                            23
a  Local Time Step      4.2278e-08                        281638


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5823          5.0002         0.50324         0.11508
v  Velocity[Y]             -4.6044          6.7283         0.37514          0.2724
v  Velocity[Z]             -7.7464          4.4231        -0.29766      -0.0016672
v  ǁVelocityǁ            0.0029685           8.821          1.8008          2.2415
v  Pressure                -2142.6           26587           17631           14328
a  k                   -0.00042169                            14
a  epsilon                 -28.647                            23
a  Local Time Step      4.2278e-08                        281638


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5823          5.0002         0.50324         0.11508
v  Velocity[Y]             -4.6044          6.7283         0.37514          0.2724
v  Velocity[Z]             -7.7464          4.4231        -0.29766      -0.0016672
v  ǁVelocityǁ            0.0029685           8.821          1.8008          2.2415
v  Pressure                -2142.6           26587           17631           14328
v  k                    1.6573e-08         0.73121       0.0087735        0.012368
v  epsilon              3.9715e-05           23517           41.07          7.4202
v  TurbVisc             9.1105e-14         0.16883      0.00069426        0.008776
v  CourantNb              0.022502           60080          105.63          24.607
v  FourierNb               0.22305      2.3653e+06          217.56          2.8019
v  total_pressure       4.9786e+05      5.2659e+05      5.1763e+05      5.1433e+05
v  Local Time Step            0.01         0.15766        0.010005        0.010046


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6263      2.3753e+06          323.19          27.409


 TIME FOR THE TIME STEP              254:        0.14110E+03

===============================================================


 INSTANT    0.255000000E+02   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        -0.108014004E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441864E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24940E+01 0.19015E+01
   Friction velocity        uet   :  0.19023E-01 0.16286E+02
   Friction velocity        uk    :  0.19002E-01 0.16286E+02
   Dimensionless distance   yplus :  0.15535E-02 0.10106E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3875
   Nb of faces within the viscous sub-layer     :      24475
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67997E+00     367   0.19352E+00   0.22770E+00 0.20353E+01 
c  Velocity[X]                                      0.68096E-01 
c  Velocity[Y]                                      0.83259E-01 
c  Velocity[Z]                                      0.76346E-01 
c  Pressure     0.25006E-01     829   0.10702E-01   0.33685E-01 0.23396E-01 
c  k            0.26713E-01     140   0.20935E-03   0.20771E-04 0.19364E+01 
c  epsilon      0.23030E+03     105   0.39194E-03   0.16143E+04 0.66635E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00042161                            10
a  epsilon                -0.44784                            16
a  Local Time Step      4.2278e-08                        281643


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5489          4.9893         0.50357         0.11513
v  Velocity[Y]             -4.5956          6.8632         0.37552         0.27243
v  Velocity[Z]             -7.7512          4.4065        -0.29838       -0.001626
v  ǁVelocityǁ            0.0015556          8.8095          1.8013          2.2411
v  Pressure                -2129.9           26590           17634           14330
v  k                    1.4607e-08         0.73346       0.0087665         0.01237
v  epsilon              7.5296e-05           23613          41.099          7.4262
v  TurbVisc             1.0775e-13         0.16883      0.00069463       0.0087759
v  CourantNb              0.070928           55987          105.74          24.609
v  FourierNb               0.22305      2.3653e+06          217.56          2.8017
v  total_pressure       4.9787e+05      5.2659e+05      5.1763e+05      5.1433e+05
v  Local Time Step            0.01         0.15766        0.010005        0.010046


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier     Dimensionless distance   yplus :  0.14293E-02 0.10171E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3875
   Nb of faces within the viscous sub-layer     :      24463
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67985E+00     368   0.19211E+00   0.23024E+00 0.20465E+01 
c  Velocity[X]                                      0.65725E-01 
c  Velocity[Y]                     Dimensionless distance   yplus :  0.14293E-02 0.10171E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3875
   Nb of faces within the viscous sub-layer     :      24463
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67985E+00     368   0.19211E+00   0.23024E+00 0.20465E+01 
c  Velocity[X]                                      0.65725E-01 
c  Velocity[Y]                      Dimensionless distance   yplus :  0.14293E-02 0.10171E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3875
   Nb of faces within the viscous sub-layer     :      24463
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67985E+00     368   0.19211E+00   0.23024E+00 0.20465E+01 
c  Velocity[X]                                      0.65725E-01 
c  Velocity[Y]                                      0.87922E-01 
c  Velocity[Z]                                      0.76592E-01 
c  Pressure     0.24868E-01     687   0.10501E-01   0.33492E-01 0.14263E-01 
c  k            0.26718E-01     138   0.33306E-03   0.21068E-04 0.19501E+01 
c  epsilon      0.22951E+03      99   0.44125E-03   0.32313E+04 0.93792E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00040081                            19
a  epsilon                 -23.958                            32
a  Local Time Step      4.2278e-08                        281644


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5909          4.9941         0.50378         0.11515
v  Velocity[Y]             -4.6077          6.7146         0.37465         0.27248
v  Velocity[Z]              -7.686          4.4071        -0.29752      -0.0015983
v  ǁVelocityǁ            0.0020518          8.7558          1.8006          2.2412
v  Pressure                  -2123           26590           17636           14330
v  k                    1.7341e-08         0.72786       0.0087889        0.012369
v  epsilon              5.9068e-05           23351          41.214          7.4345
v  TurbVisc             8.9721e-14         0.16883       0.0006938        0.008776
v  CourantNb              0.032368           56614          105.88          24.605
v  FourierNb               0.22305      2.3653e+06          217.56          2.8013
v  total_pressure       4.9788e+05      5.2659e+05      5.1764e+05      5.1433e+05
v  Local Time Step            0.01         0.15767        0.010005        0.010046


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6441      2.3758e+06          323.44          27.406


 TIME FOR THE TIME STEP              256:        0.13458E+03

===============================================================


 INSTANT    0.257000000E+02   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        -0.986829595E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441228E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24689E+01 0.19032E+01
   Friction velocity        uet   :  0.21293E-01 0.15479E+02
   Friction velocity        uk    :  0.21151E-01 0.15479E+02
   Dimensionless distance   yplus :  0.17294E-02 0.10231E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3880
   Nb of faces within the viscous sub-layer     :      24485
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67988E+00     367   0.19331E+00   0.22417E+00 0.20197E+01 
c  Velocity[X]                                      0.63566E-01 
c  Velocity[Y]                                      0.85453E-01 
c  Velocity[Z]                                      0.75153E-01 
c  Pressure     0.24815E-01     832   0.10407E-01   0.33427E-01 0.23190E-01 
c  k            0.26736E-01     135   0.19944E-03   0.16092E-04 0.17046E+01 
c  epsilon      0.23295E+03     106   0.36135E-03   0.18826E+04 0.71694E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00044453                            22
a  epsilon                 -1.7604                            38
a  Local Time Step      4.2278e-08                    INSTANT    0.258000000E+02   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        -0.469270635E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441232E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+0 INSTANT    0.258000000E+02   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        -0.469270635E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441232E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00 INSTANT    0.258000000E+02   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        -0.469270635E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441232E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24654E+01 0.19058E+01
   Friction velocity        uet   :  0.21494E-01 0.15362E+02
   Friction velocity        uk    :  0.21197E-01 0.15362E+02
   Dimensionless distance   yplus :  0.18441E-02 0.10267E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3873
   Nb of faces within the viscous sub-layer     :      24467
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67981E+00     366   0.19402E+00   0.22213E+00 0.20105E+01 
c  Velocity[X]                                      0.65149E-01 
c  Velocity[Y]                                      0.81034E-01 
c  Velocity[Z]                                      0.75943E-01 
c  Pressure     0.24360E-01     617   0.10199E-01   0.32833E-01 0.15866E-01 
c  k            0.26728E-01     132   0.19433E-03   0.19061E-04 0.18549E+01 
c  epsilon      0.22984E+03     114   0.37277E-03   0.16289E+04 0.66652E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00041185                            11
a  epsilon                 -26.835                            25
a  Local Time Step      4.2278e-08                        281650


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5799          4.9765         0.50387          0.1151
v  Velocity[Y]              -4.607          6.7179         0.37577         0.27246
v  Velocity[Z]             -7.7685          4.4321        -0.29813       -0.001584
v  ǁVelocityǁ            0.0034989          8.8282          1.8012          2.2409
v  Pressure                -2119.3           26592           17639           14332
v  k                    1.8468e-08         0.73113       0.0087885        0.012365
v  epsilon              5.8333e-05           23514          41.119          7.4338
v  TurbVisc             1.0285e-13         0.16883      0.00069424       0.0087754
v  CourantNb              0.071013           51462          105.81          24.601
v  FourierNb               0.22307      2.3653e+06          217.56          2.8013
v  total_pressure       4.9788e+05      5.2659e+05      5.1764e+05      5.1433e+05
v  Local Time Step            0.01         0.11695        0.010005        0.010045


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.642      2.3768e+06          323.37          27.402


 TIME FOR THE TIME STEP              258:        0.13018E+03

===============================================================


 INSTANT    0.259000000E+02   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         0.148088822E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441847E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24506E+01 0.19005E+01
   Friction velocity        uet   :  0.18548E-01 0.16841E+02
   Friction velocity        uk    :  0.18773E-01 0.16841E+02
   Dimensionless distance   yplus :  0.17605E-02 0.10286E+02
   ------------------------------------------------------
   Nb of reversal of the-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5323           4.993         0.50371         0.11505
v  Velocity[Y]             -4.6061           6.839         0.37595         0.27238
v  Velocity[Z]               -7.75          4.3835         -0.2984      -0.0015818
v  ǁVelocityǁ            0.0032439          8.7976           1.801          2.2409
v  Pressure                -2127.1           26591           17640           14333
v  k                    1.6088e-08         0.73134       0.0087852        0.012364
v  epsilon              8.4453e-05           23535          41.342          7.4356
v  TurbVisc             1.1828e-13         0.16883      0.00069497       0.0087751
v  CourantNb              0.024182           48248          105.83            24.6
v  Fouri-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5323           4.993         0.50371         0.11505
v  Velocity[Y]             -4.6061           6.839         0.37595         0.27238
v  Velocity[Z]               -7.75          4.3835         -0.2984      -0.0015818
v  ǁVelocityǁ            0.0032439          8.7976           1.801          2.2409
v  Pressure                -2127.1           26591           17640           14333
v  k                    1.6088e-08         0.73134       0.0087852        0.012364
v  epsilon              8.4453e-05           23535          41.342          7.4356
v  TurbVisc             1.1828e-13         0.16883      0.00069497       0.0087751
v  CourantNb              0.024182           48248          105.83            24.6
v  Fourie-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5323           4.993         0.50371         0.11505
v  Velocity[Y]             -4.6061           6.839         0.37595         0.27238
v  Velocity[Z]               -7.75          4.3835         -0.2984      -0.0015818
v  ǁVelocityǁ            0.0032439          8.7976           1.801          2.2409
v  Pressure                -2127.1           26591           17640           14333
v  k                    1.6088e-08         0.73134       0.0087852        0.012364
v  epsilon              8.4453e-05           23535          41.342          7.4356
v  TurbVisc             1.1828e-13         0.16883      0.00069497       0.0087751
v  CourantNb              0.024182           48248          105.83            24.6
v  FourierNb                0.2231      2.3653e+06          217.57          2.8016
v  total_pressure       4.9787e+05      5.2659e+05      5.1764e+05      5.1433e+05
v  Local Time Step            0.01         0.12864        0.010005        0.010046


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6445      2.3799e+06           323.4          27.402


 TIME FOR THE TIME STEP              259:        0.13330E+03

===============================================================


 INSTANT    0.260000000E+02   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        -0.104918444E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441274E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24444E+01 0.19018E+01
   Friction velocity        uet   :  0.17638E-01 0.18237E+02
   Friction velocity        uk    :  0.17411E-01 0.18237E+02
   Dimensionless distance   yplus :  0.18456E-02 0.10287E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3878
   Nb of faces within the viscous sub-layer     :      24472
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67995E+00     362   0.19268E+00   0.21768E+00 0.19902E+01 
c  Velocity[X]                                      0.60551E-01 
c  Velocity[Y]                                      0.81224E-01 
c  Velocity[Z]                                      0.75906E-01 
c  Pressure     0.23917E-01     889   0.98888E-02   0.32252E-01 0.35808E-01 
c  k            0.26724E-01     129   0.21811E-03   0.19129E-04 0.18584E+01 
c  epsilon      0.22978E+03     122   0.41494E-03   0.34313E+04 0.96730E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00040183                            30
a  epsilon                 -27.946                            49
a  Local Time Step      4.2278e-08                        281646


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5273          4.9666         0.50324         0.11502
v  Velocity[Y]             -4.6021          6.8056         0.37617         0.27243
v  Velocity[Z]             -7.7679          4.7603        -0.29966      -0.0015783
v  ǁVelocityǁ            0.0020193          8.8111          1.8018           2.241
v  Pressure                -2133.3           26583           17633           14328
v  k                    1.6024e-08         0.72928       0.0087796        0.012363
v  epsilon              7.0488e-05           23423          41.163          7.4316
v  TurbVisc             1.0039e-13         0.16883      0.00069505       0.0087749
v  CourantNb              0.041362           47002          105.77            24.6
v  FourierNb               0.22312      2.3653e+06          217.57          2.8019
v  total_pressure       4.9787e+05      5.2658e+05      5.1763e+05      5.1433e+05
v  Local Time Step            0.01          0.1415        0.010005        0.010047


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6529        2.38e+06          323.34          27.402


 TIME FOR THE TIME STEP              260:        0.14804E+03

===============================================================


 INSTANT    0.261000000E+02   TIME STEP NUMBER             261
 =============================================------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68034E+00     370   0.19368E+00   0.21721E+00 0.19883E+01 
c  Velocity[X]                                      0.58864E-01 
c  Velocity[Y]                                      0.80591E-01 
c  Velocity[Z]                                      0.77753E-01 
c  Pressure     0.23302E-01     811   0.96646E-02   0.31429E-01 0.24305E-01 
c  k            0.26747E-01     131   0.17643E-03   0.14633E-04 0.16251E+01 
c  epsilon      0.23255E+03     114   0.36300E-03 ------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68034E+00     370   0.19368E+00   0.21721E+00 0.19883E+01 
c  Velocity[X]                                      0.58864E-01 
c  Velocity[Y]                                      0.80591E-01 
c  Velocity[Z]                                      0.77753E-01 
c  Pressure     0.23302E-01     811   0.96646E-02   0.31429E-01 0.24305E-01 
c  k            0.26747E-01     131   0.17643E-03   0.14633E-04 0.16251E+01 
c  epsilon      0.23255E+03     114   0.36300E-03  ------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68034E+00     370   0.19368E+00   0.21721E+00 0.19883E+01 
c  Velocity[X]                                      0.58864E-01 
c  Velocity[Y]                                      0.80591E-01 
c  Velocity[Z]                                      0.77753E-01 
c  Pressure     0.23302E-01     811   0.96646E-02   0.31429E-01 0.24305E-01 
c  k            0.26747E-01     131   0.17643E-03   0.14633E-04 0.16251E+01 
c  epsilon      0.23255E+03     114   0.36300E-03   0.16096E+04 0.66134E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00045667                            13
a  epsilon                -0.95747                            21
a  Local Time Step      4.2278e-08                        281644


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5595          4.9685         0.50324         0.11497
v  Velocity[Y]             -4.5875          6.7746          0.3762         0.27241
v  Velocity[Z]             -7.7728          4.4028        -0.29944      -0.0015105
v  ǁVelocityǁ            0.0028514          8.8175           1.802          2.2408
v  Pressure                  -2135           26588           17637           14331
v  k                    1.5705e-08         0.73434       0.0087861        0.012364
v  epsilon              5.6132e-05           23673          41.222          7.4387
v  TurbVisc             1.0236e-13         0.16883      0.00069501       0.0087747
v  CourantNb               0.12191           42909           105.8          24.602
v  FourierNb               0.22313      2.3653e+06          217.56          2.8015
v  total_pressure       4.9787e+05      5.2659e+05      5.1764e+05      5.1433e+05
v  Local Time Step            0.01         0.15565        0.010005        0.010046


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6553      2.3796e+06          323.36          27.404


 TIME FOR THE TIME STEP              261:        0.14087E+03

===============================================================


 INSTANT    0.262000000E+02   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        -0.249516918E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441241E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24418E+01 0.19053E+01
   Friction velocity        uet   :  0.18092E-01 0.20708E+02
   Friction velocity        uk    :  0.18071E-01 0.20708E+02
   Dimensionless distance   yplus :  0.18652E-02 0.10286E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3882
   Nb of faces within the viscous sub-layer     :      24459
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68008E+00     377   0.19656E+00   0.21329E+00 0.19702E+01 
c  Velocity[X]                                      0.61798E-01 
c  Velocity[Y]                                      0.77776E-01 
c  Velocity[Z]                                      0.73715E-01 
c  Pressure     0.22823E-01     728   0.94604E-02   0.30791E-01 0.14687E-01 
c  k            0.26724E-01     130   0.20483E-03   0.20291E-04 0.19139E+01 
c  epsilon      0.22963E+03     112   0.38206E-03   0.17926E+04 0.69991E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00043902                            22
a  epsilon                 -25.571                            32
a  Local Time Step      4.2278e-08                        281649


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.702462278E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441858E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ----------------------------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.702462278E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441858E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   -----------------------------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.702462278E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441858E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24383E+01 0.18992E+01
   Friction velocity        uet   :  0.14958E-01 0.22149E+02
   Friction velocity        uk    :  0.14782E-01 0.22149E+02
   Dimensionless distance   yplus :  0.17780E-02 0.10278E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3885
   Nb of faces within the viscous sub-layer     :      24472
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67977E+00     371   0.19098E+00   0.22150E+00 0.20077E+01 
c  Velocity[X]                                      0.63434E-01 
c  Velocity[Y]                                      0.80845E-01 
c  Velocity[Z]                                      0.77219E-01 
c  Pressure     0.23373E-01     760   0.95700E-02   0.31535E-01 0.15199E-01 
c  k            0.26741E-01     133   0.19873E-03   0.15588E-04 0.16776E+01 
c  epsilon      0.23295E+03     121   0.44114E-03   0.13306E+04 0.60290E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.702462278E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441858E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24383E+01 0.18992E+01
   Friction velocity        uet   :  0.14958E-01 0.22149E+02
   Friction velocity        uk    :  0.14782E-01 0.22149E+02
   Dimensionless distance   yplus :  0.17780E-02 0.10278E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3885
   Nb of faces within the viscous sub-layer     :      24472
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67977E+00     371   0.19098E+00   0.22150E+00 0.20077E+01 
c  Velocity[X]                                      0.63434E-01 
c  Velocity[Y]                                      0.80845E-01 
c  Velocity[Z]                                      0.77219E-01 
c  Pressure     0.23373E-01     760   0.95700E-02   0.31535E-01 0.15199E-01 
c  k            0.26741E-01     133   0.19873E-03   0.15588E-04 0.16776E+01 
c  epsilon      0.23295E+03     121   0.44114E-03   0.13306E+04 0.60290E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00046932                            25
a  epsilon                 -1.7212                            36
a  Local Time Step      4.2278e-08                        281644


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5552          4.9913         0.50423         0.11492
v  Velocity[Y]             -4.5838          6.7533         0.37529         0.27242
v  Velocity[Z]             -7.7501          4.3686        -0.29881      -0.0014991
v  ǁVelocityǁ            0.0035606          8.8267          1.8017          2.2409
v  Pressure                -2146.1           26582           17633           14328
v  k                    1.5844e-08         0.73008       0.0087709        0.012364
v  epsilon               9.535e-05           23480          41.006          7.4324
v  TurbVisc             1.0203e-13         0.16883      0.00069639       0.0087747
v  CourantNb              0.038878           37893          105.72          24.599
v  FourierNb               0.22311      2.3653e+v  Velocity[Z]             -7.7517          4.4068        -0.29838       -0.001487
v  ǁVelocityǁ            0.0024871          8.8221          1.8013          2.2405
v  Pressure                -2146.9           26582           17634           14328
v  k                    1.4505e-08         0.73126       0.0087921        0.012365
v  epsilon              9.0422e-05           23529          41.189          7.4323
v  TurbVisc             9.7896e-14         0.16883      0.00069666       0.0087746
v  CourantNb               0.10834           37996          105.78          24.601
v  FourierNb                0.2231      2.3653e+06          217.56           2.802
v  total_pressure       4.9785e+05      5.2658e+05      5.1763e+05      5.1433e+05
v  Local Time Step            0.01         0.15768        0.010006        0.010048


  ** Cv  Velocity[Z]             -7.7517          4.4068        -0.29838       -0.001487
v  ǁVelocityǁ            0.0024871          8.8221          1.8013          2.2405
v  Pressure                -2146.9           26582           17634           14328
v  k                    1.4505e-08         0.73126       0.0087921        0.012365
v  epsilon              9.0422e-05           23529          41.189          7.4323
v  TurbVisc             9.7896e-14         0.16883      0.00069666       0.0087746
v  CourantNb               0.10834           37996          105.78          24.601
v  FourierNb                0.2231      2.3653e+06          217.56           2.802
v  total_pressure       4.9785e+05      5.2658e+05      5.1763e+05      5.1433e+05
v  Local Time Step            0.01         0.15768        0.010006        0.010048


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6766      2.3777e+06          323.34          27.403


 TIME FOR THE TIME STEP              264:        0.13416E+03

===============================================================


 INSTANT    0.265000000E+02   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        -0.149929640E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441256E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24368E+01 0.19023E+01
   Friction velocity        uet   :  0.17197E-01 0.21882E+02
   Friction velocity        uk    :  0.17180E-01 0.21882E+02
   Dimensionless distance   yplus :  0.17788E-02 0.10257E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3882
   Nb of faces within the viscous sub-layer     :      24462
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67974E+00     376   0.19400E+00   0.21973E+00 0.19997E+01 
c  Velocity[X]                                      0.62309E-01 
c  Velocity[Y]                                      0.82270E-01 
c  Velocity[Z]                                      0.75149E-01 
c  Pressure     0.23016E-01     831   0.94944E-02   0.31060E-01 0.19428E-01 
c  k            0.26733E-01     133   0.19824E-03   0.15811E-04 0.16893E+01 
c  epsilon      0.23330E+03     104   0.43394E-03   0.14007E+04 0.61891E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00046708                            12
a  epsilon                 -3.0293                            21
a  Local Time Step      4.2278e-08                        281641


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5465          4.9818         0.50422         0.11485
v  Velocity[Y]             -4.5968          6.7452         0.37544         0.27249
v  Velocity[Z]             -7.7592          4.3761        -0.29885      -0.0015345
v  ǁVelocityǁ            0.0021106          8.8256          1.8014          2.2407
v  Pressure                -2154.3         v  Velocity[Z]             -7.7517          4.4068        -0.29838       -0.001487
v  ǁVelocityǁ            0.0024871          8.8221          1.8013          2.2405
v  Pressure                -2146.9           26582           17634           14328
v  k                    1.4505e-08         0.73126       0.0087921        0.012365
v  epsilon              9.0422e-05           23529          41.189          7.4323
v  TurbVisc             9.7896e-14         0.16883      0.00069666       0.0087746
v  CourantNb               0.10834           37996          105.78          24.601
v  FourierNb                0.2231      2.3653e+06          217.56           2.802
v  total_pressure       4.9785e+05      5.2658e+05      5.1763e+05      5.1433e+05
v  Local Time Step            0.01         0.15768        0.010006        0.010048


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6766      2.3777e+06          323.34          27.403


 TIME FOR THE TIME STEP              264:        0.13960E+03

===============================================================


 INSTANT    0.265000000E+02   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        -0.149929640E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441256E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
------------------------------------------------------------------------------------------------------------------------------------
c  Velocity     0.68011E+00     360   0.19631E+00   0.21900E+00 0.19962E+01 
c  Velocity[X]                                      0.61307E-01 
c  Velocity[Y]                                      0.82550E-01 
c  Velocity[Z]                                      0.75144E-01 
c  Pressure     0.23920E-01     870   0.98546E-02   0.32270E-01 0.31527E-01 
c  k            0.26719E-01     129   0.20895E-03   0.15969E-04 0.16975E+01 
c  epsilon      0.22980E+03      95   0.40380E-03   0.13711E+04 0.61149E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  ---------------------------------------------------------------------------------
c  Velocity     0.68011E+00     360   0.19631E+00   0.21900E+00 0.19962E+01 
c  Velocity[X]                                      0.61307E-01 
c  Velocity[Y]                                      0.82550E-01 
c  Velocity[Z]                                      0.75144E-01 
c  Pressure     0.23920E-01     870   0.98546E-02   0.32270E-01 0.31527E-01 
c  k            0.26719E-01     129   0.20895E-03   0.15969E-04 0.16975E+01 
c  epsilon      0.22980E+03      95   0.40380E-03   0.13711E+04 0.61149E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00042668                            26
a  epsilon                 -25.914                            43
a  Local Time Step      4.2278e-08                        281643


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5661          4.9595         0.50398         0.11487
v  Velocity[Y]             -4.5957          6.7572         0.37556         0.27251
v  Velocity[Z]             -7.7095          4.4198        -0.29892       -0.001541
v  ǁVelocityǁ            0.0039713          8.7823          1.8021          2.2409
v  Pressure                -2168.3           26578           17631           14326
v  k                    1.4636e-08         0.73119       0.0088053        0.012368
v  epsilon              6.7301e-05           23544          41.233          7.4356
v  TurbVisc             9.3626e-14         0.16883      0.00069785       0.0087749
v  CourantNb              0.036017           37893          105.84          24.598
v  FourierNb               0.22305      2.3653e+06          217.56           2.802
v  total_pressure       4.9783e+05      5.2658e+05      5.1763e+05      5.1433e+05
v  Local Time Step            0.01         0.15768        0.010005        0.010045


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6692      2.3792e+06           323.4            27.4


 TIME FOR THE TIME STEP              266:        0.14754E+03

===============================================================


 INSTANT    0.267000000E+02   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         0.143399132E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441845E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24479E+01 0.19043E+01
   Friction velocity        uet   :  0.19565E-01 0.19989E+02
   Friction velocity        uk    :  0.19907E-01 0.19989E+02
   Dimensionless distance   yplus :  0.18295E-02 0.10128E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3880
   Nb of faces within the viscous sub-layer     :      24458
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68021E+00     366   0.19443E+00   0.21281E+00 0.19678E+01 
c  Velocity[X]                                      0.62-----------------------------------------------------------------------------
c  Velocity     0.68011E+00     360   0.19631E+00   0.21900E+00 0.19962E+01 
c  Velocity[X]                                      0.61307E-01 
c  Velocity[Y]                                      0.82550E-01 
c  Velocity[Z]                                      0.75144E-01 
c  Pressure     0.23920E-01     870   0.98546E-02   0.32270E-01 0.31527E-01 
c  k            0.26719E-01     129   0.20895E-03   0.15969E-04 0.16975E+01 
c  epsilon      0.22980E+03      95   0.40380E-03   0.13711E+04 0.61149E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00042668                            26
a  epsilon                 -25.914                            43
a  Local Time Step      4.2278e-08                        281643


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5661          4.9595         0.50398         0.11487
v  Velocity[Y]             -4.5957          6.7572         0.37556         0.27251
v  Velocity[Z]             -7.7095          4.4198        -0.29892       -0.001541
v  ǁVelocityǁ            0.0039713          8.7823          1.8021          2.2409
v  Pressure                -2168.3           26578           17631           14326
v  k                    1.4636e-08         0.73119       0.0088053        0.012368
v  epsilon              6.7301e-05           23544          41.233          7.4356
v  TurbVisc             9.3626e-14         0.16883      0.00069785       0.0087749
v  CourantNb              0.036017           37893          105.84          24.598
v  FourierNb               0.22305      2.3653e+06          217.56           2.802
v  total_pressure       4.9783e+05      5.2658e+05      5.1763e+05      5.1433e+05
v  Local Time Step            0.01         0.15768        0.Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441237E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24448E+01 0.19071E+01
   Friction velocity        uet   :  0.15960E-01 0.18994E+02Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441237E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24448E+01 0.19071E+01
   Friction velocity        uet   :  0.15960E-01 0.18994E+02
   Friction velocity        uk    :  0.15942E-01 0.18994E+02
   Dimensionless distance   yplus :  0.18092E-02 0.10176E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3875
   Nb of faces within the viscous sub-layer     :      24452
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67981E+00     378   0.19031E+00   0.22046E+00 0.20030E+01 
c  Velocity[X]                                      0.64693E-01 
c  Velocity[Y]                                      0.80859E-01 
c  Velocity[Z]                                      0.74904E-01 
c  Pressure     0.22902E-01     652   0.93905E-02   0.30900E-01 0.14394E-01 
c  k            0.26715E-01     127   0.19528E-03   0.15252E-04 0.16592E+01 
c  epsilon      0.22972E+03     103   0.38438E-03   0.14071E+04 0.62056E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00044493                            15
a  epsilon                 -27.142                            35
a  Local Time Step      4.2278e-08                        281644


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5701           4.986         0.50488         0.11489
v  Velocity[Y]             -4.6088          6.7709         0.37512         0.27251
v  Velocity[Z]             -7.7475          4.4062        -0.29778      -0.0014716
v  ǁVelocityǁ           0.00082287          8.8103          1.8012          2.2406
v  Pressure                -2188.6           26584           17636           14329
v  k                    1.4617e-08         0.73104       0.0087904        0.012369
v  epsilon              6.0482e-05           23533          41.011          7.4302
v  TurbVisc              9.494e-14         0.16883      0.00069991        0.008776
v  CourantNb              0.021148           38403          105.88            24.6
v  FourierNb               0.22305      2.3653e+06          217.56          2.8022
v  total_pressure       4.9781e+05      5.2658e+05      5.1764e+05      5.1433e+05
v  Local Time Step            0.01         0.15768        0.010005        0.010047


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6421      2.3793e+06          323.44          27.402


 TIME FOR THE TIME STEP              268:        0.13485E+03

===============================================================


 INSTANT    0.269000000E+02   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        -0.605583562E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441244E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24374E+01 0.19048E+01
   Friction velocity        uet   :  0.13110E-01 0.17920E+02
   Friction velocity        uk    :  0.14120E-01 0.17920E+02
   Dimensionless distance   yplus :  0.18524E-02 0.10277E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3883
   Nb of faces within the viscous sub-layer     :      24463
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67987E+00     369   0.18865E+00   0.22202E+00 0.20101E+01 
c  Velocity[X]                                      0.62495E-01 
c  Velocity[Y]                                      0.84489E-01 
c  Velocity[Z]                                      0.75035E-01 
c  Pressure     0.23235E-01     776   0.94641E-02   0.31370E-01 0.15972E-01 
c  k            0.26733E-01     131   0.16479E-03   0.15614E-04 0.16785E+01 
c  epsilon      0.23269E+03     117   0.38176E-03   0.15170E+04 0.64304E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00047279                            22
a  epsilon         v  epsilon              1.8653e-05           23633          41.436          7.4357
v  TurbVisc             9.1177e-14         0.16883      0.00070097       0.0087768
v  CourantNb              0.090478           38904          105.73            24.6
v  FourierNb               0.22305      2.3653e+06          217.56          2.8023
v  total_pressure       4.9781e+05      5.2659e+05      5.1764e+05      5.1433e+05
v  Local Time Step            0.01         0.13055        0.010005        0.010047


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6604      2.3776e+06          323.29          27.402


 TIME FOR THE TIME STEP     v  epsilon              1.8653e-05           23633          41.436          7.4357
v  TurbVisc             9.1177e-14         0.16883      0.00070097       0.0087768
v  CourantNb              0.090478           38904          105.73            24.6
v  FourierNb               0.22305      2.3653e+06          217.56          2.8023
v  total_pressure       4.9781e+05      5.2659e+05      5.1764e+05      5.1433e+05
v  Local Time Step            0.01         0.13055        0.010005        0.010047


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6604      2.3776e+06          323.29          27.402


 TIME FOR THE TIME STEP              269:        0.14139E+03

===============================================================


 INSTANT    0.270000000E+02   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        -0.414028612E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441235E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24331E+01 0.19027E+01
   Friction velocity        uet   :  0.16993E-01 0.17045E+02
   Friction velocity        uk    :  0.17539E-01 0.17045E+02
   Dimensionless distance   yplus :  0.16553E-02 0.10297E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3877
   Nb of faces within the viscous sub-layer     :      24469
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68037E+00     363   0.19199E+00   0.21313E+00 0.19694E+01 
c  Velocity[X]                                      0.60634E-01 
c  Velocity[Y]                                      0.80545E-01 
c  Velocity[Z]                                      0.71954E-01 
c  Pressure     0.22381E-01     837   0.92084E-02   0.30220E-01 0.20650E-01 
c  k            0.26726E-01     126   0.19720E-03   0.17148E-04 0.17591E+01 
c  epsilon      0.23030E+03     112   0.41825E-03   0.31140E+04 0.91866E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00042732                            15
a  epsilon                 -26.286                            32
a  Local Time Step      4.2278e-08                        281647


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]               -2.53          4.9858         0.50478         0.11489
v  Velocity[Y]             -4.5968          6.7038         0.37616         0.27242
v  Velocity[Z]             -7.7416          4.4161          -0.298      -0.0015001
v  ǁVelocityǁ            0.0020314          8.8122          1.8027          2.2408
v  Pressure                -2197.5           26592           17643           14333
v  k                    1.4314e-08         0.72831       0.0088015        0.012371
v  epsilon              2.4208e-05           23407          41.335          7.4376
v  TurbVisc             5.8016e-14         0.16883      0.00070088       0.0087768
v  CourantNb               0.01531           39210          105.72          24.599
v  FourierNb               0.22306      2.3653e+06          217.56          2.8025
v  total_pressure        4.978e+05      5.2659e+05      5.1764e+05      5.1433e+05
v  Local Time Step            0.01         0.13346        0.010006        0.010049


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6597       2.379e+06          323.28          27.401


 TIME FOR THE TIME STEP              270:        0.14156E+03

===============================================================


 INSTANT    0.271000000E+02   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        -0.600595321E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441232E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24182E+01 0.19043E+01
   Friction velocity        uet   :  0.17216E-01 0.16925E+02
   Friction velocity        uk    :  0.17727E-01 0.16925E+02
   Dimensionless distance   yplusc  Velocity[Z]                                      0.75782E-01 
c  Pressure     0.23282E-01     870   0.95043E-02   0.31432E-01 0.25602E-01 
c  k            0.26742E-01     131   0.20601E-03   0.17515E-04 0.17776E+01 
c  epsilon      0.23352E+03     108   0.46815E-03   0.32459E+04 0.93986E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0004715                            12
a  epsilon                 -1.0708                            23
a  Local Time Step      4.2278e-08                        281648


  ** Computed fields on cells
   c  Velocity[Z]                                      0.75782E-01 
c  Pressure     0.23282E-01     870   0.95043E-02   0.31432E-01 0.25602E-01 
c  k            0.26742E-01     131   0.20601E-03   0.17515E-04 0.17776E+01 
c  epsilon      0.23352E+03     108   0.46815E-03   0.32459E+04 0.93986E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0004715                            12
a  epsilon                 -1.0708                            23
a  Local Time Step      4.2278e-08                        281648


  ** Computed fields on cells
    c  Velocity[Z]                                      0.75782E-01 
c  Pressure     0.23282E-01     870   0.95043E-02   0.31432E-01 0.25602E-01 
c  k            0.26742E-01     131   0.20601E-03   0.17515E-04 0.17776E+01 
c  epsilon      0.23352E+03     108   0.46815E-03   0.32459E+04 0.93986E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0004715                            12
a  epsilon                 -1.0708                            23
a  Local Time Step      4.2278e-08                        281648


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5395          5.0234         0.50438         0.11476
v  Velocity[Y]              -4.601          6.7734          0.3758         0.27241
v  Velocity[Z]             -7.7524          4.5707        -0.29812      -0.0014897
v  ǁVelocityǁ            0.0029137          8.8194          1.8025          2.2409
v  Pressure                  -2196           26597           17649           14337
v  k                    1.5141e-08         0.73367       0.0088025        0.012374
v  epsilon              9.0305e-05           23686          41.207          7.4415
v  TurbVisc             8.9607e-14         0.16883        0.000702       0.0087775
v  CourantNb              0.014482           38188          105.89          24.602
v  FourierNb               0.22308      2.3653e+06          217.56          2.8023
v  total_pressure        4.978e+05       5.266e+05      5.1765e+05      5.1434e+05
v  Local Time Step            0.01          0.1468        0.010005        0.010044


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6651      2.3825e+06          323.46          27.404


 TIME FOR THE TIME STEP              271:        0.14871E+03

===============================================================


 INSTANT    0.272000000E+02   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        -0.104426057E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441236E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24187E+01 0.19101E+01
   Friction velocity        uet   :  0.20551E-01 0.15708E+02
   Friction velocity        uk    :  0.20527E-01 0.15708E+02
   Dimensionless distance   yplus :  0.16972E-02 0.10309E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3876
   Nb of faces within the viscous sub-layer     :      24462
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68082E+00     380   0.19501E+00   0.21102E+00 0.19598E+01 
c  Velocity[X]                                      0.59957E-01 
c  Velocity[Y]                                      0.77228E-01 
c  Velocity[Z]                                      0.73833E-01 
c  Pressure     0.23046E-01     889   0.94444E-02   0.31128E-01 0.31058E-01 
c  k            0.26722E-01     127   0.18570E-03   0.13722E-04 0.15736E+01 
c  epsilon      0.22984E+03     117   0.40664E-03   0.12289E+04 0.57951E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00043441                            27
a  epsilon                 -26.789                            45
a  Local Time Step      4.2278e-08                        281646


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.4831           5.002         0.50475         0.11476
v  Velocity[Y]             -4.6002          6.6814         0.37533         0.27237
v  Velocity[Z]             -7.6637          4.3965        -0.29793      -0.0015234
v  ǁVelocityǁ            0.0023827          8.7313           1.803          2.2406
v  Pressure                  -2191           26607           17656           14341
v  k                    1.4717e-08         0.73208       0.0088033        0.012373
v  epsilon              0.00021329           23577           41.23          7.4336
v  TurbVisc       Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24174E+01 0.19002E+01
   Friction velocity        uet   :  0.21736E-01 0.15815E+02
   Friction velocity        uk    :  0.21238E-01 0.15815E+02
   Dimensionless distance   yplus :  0.14898E-02 0.10317E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3878
   Nb of facesFree surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24174E+01 0.19002E+01
   Friction velocity        uet   :  0.21736E-01 0.15815E+02
   Friction velocity        uk    :  0.21238E-01 0.15815E+02
   Dimensionless distance   yplus :  0.14898E-02 0.10317E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3878
   Nb of faces Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24174E+01 0.19002E+01
   Friction velocity        uet   :  0.21736E-01 0.15815E+02
   Friction velocity        uk    :  0.21238E-01 0.15815E+02
   Dimensionless distance   yplus :  0.14898E-02 0.10317E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3878
   Nb of faces within the viscous sub-layer     :      24473
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68015E+00     360   0.19459E+00   0.21430E+00 0.19747E+01 
c  Velocity[X]                                      0.63997E-01 
c  Velocity[Y]                                      0.76048E-01 
c  Velocity[Z]                                      0.74258E-01 
c  Pressure     0.23356E-01     925   0.97009E-02   0.31545E-01 0.42139E-01 
c  k            0.26748E-01     131   0.15832E-03   0.14741E-04 0.16307E+01 
c  epsilon      0.23298E+03     116   0.25456E-03   0.13269E+04 0.60055E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00046674                            12
a  epsilon                -0.51344                            22
a  Local Time Step      4.2278e-08                        281651


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5459          5.0013         0.50483         0.11472
v  Velocity[Y]             -4.5961          6.7972         0.37536         0.27233
v  Velocity[Z]             -7.7674          4.5416        -0.29792      -0.0014485
v  ǁVelocityǁ            0.0023952          8.8204          1.8032          2.2408
v  Pressure                -2186.6           26617           17665           14347
v  k                    1.5652e-08          0.7301       0.0087982        0.012374
v  epsilon              8.9913e-06           23491          41.117          7.4409
v  TurbVisc             9.2414e-14         0.16883      0.00070253        0.008778
v  CourantNb              0.054621           38003          105.98          24.601
v  FourierNb               0.22314      2.3653e+06          217.56           2.802
v  total_pressure       4.9781e+05      5.2662e+05      5.1766e+05      5.1435e+05
v  Local Time Step            0.01         0.15767        0.010005        0.010044


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6848       2.382e+06          323.54          27.403


 TIME FOR THE TIME STEP              273:        0.15270E+03

===============================================================


 INSTANT    0.274000000E+02   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        -0.216722116E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441187E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24236E+01 0.19032E+01
   Friction velocity        uet   :  0.94857E-02 0.15241E+02
   Friction velocity        uk    :  0.94292E-02 0.15241E+02
   Dimensionless distance   yplus :  0.14045E-02 0.10344E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3875
   Nb of faces within the viscous sub-layer     :      24466
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68055E+00     353   0.19285E+00   0.21775E+00 0.19904E+01 
c  Velocity[X]                                      0.58517E-01 
c  Velocity[Y]                                      0.81197E-01 
c  Velocity[Z]                                      0.78036E-01 
c  Pressure     0.23311E-01     866  v  FourierNb               0.22315      2.3653e+06          217.56          2.8021
v  total_pressure       4.9782e+05      5.2662e+05      5.1767e+05      5.1435e+05
v  Local Time Step            0.01         0.15767        0.010005        0.010044


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6585      2.3756e+06          323.46          27.406


 TIME FOR THE TIME STEP              274:        0.14651E+03

===============================================================


 INSTANT    0.275000000E+02   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        -0.116091652E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441254E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
--------------------v  FourierNb               0.22315      2.3653e+06          217.56          2.8021
v  total_pressure       4.9782e+05      5.2662e+05      5.1767e+05      5.1435e+05
v  Local Time Step            0.01         0.15767        0.010005        0.010044


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6585      2.3756e+06          323.46          27.406


 TIME FOR THE TIME STEP              274:        0.14555E+03

===============================================================


 INSTANT    0.275000000E+02   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        -0.116091652E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441254E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24189E+01 0.18993E+01
   Friction velocity        uet   :  0.21530E-01 0.14146E+02
   Friction velocity        uk    :  0.21235E-01 0.14146E+02
   Dimensionless distance   yplus :  0.14954E-02 0.10178E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3887
   Nb of faces within the viscous sub-layer     :      24470
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68052E+00     379   0.19418E+00   0.21313E+00 0.19695E+01 
c  Velocity[X]                                      0.60961E-01 
c  Velocity[Y]                                      0.80543E-01 
c  Velocity[Z]                                      0.71630E-01 
c  Pressure     0.22722E-01     693   0.93110E-02   0.30696E-01 0.13328E-01 
c  k            0.26746E-01     132   0.17089E-03   0.16028E-04 0.17004E+01 
c  epsilon      0.23278E+03     104   0.36830E-03   0.34793E+04 0.97221E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00046881                            36
a  epsilon                 -39.236                            65
a  Local Time Step      4.2278e-08                        281652


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5601          5.0123         0.50461         0.11472
v  Velocity[Y]             -4.5985          6.7773         0.37607         0.27239
v  Velocity[Z]             -7.7542          4.3855        -0.29756      -0.0014779
v  ǁVelocityǁ             0.002813          8.8086          1.8028          2.2407
v  Pressure                -2186.2           26623           17669           14349
v  k                    1.6476e-08         0.72998       0.0087979        0.012373
v  epsilon              4.3319e-05           23497          41.126          7.4418
v  TurbVisc             8.8855e-14         0.16883       0.0007019       0.0087778
v  CourantNb              0.049162           40932          105.86          24.603
v  FourierNb               0.22316      2.3653e+06          217.56          2.8022
v  total_pressure       4.9781e+05      5.2662e+05      5.1767e+05      5.1435e+05
v  Local Time Step            0.01         0.15767        0.010005        0.010045


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.652      2.3757e+06          323.42          27.405


 TIME FOR THE TIME STEP              275:        0.13826E+03

===============================================================


 INSTANT    0.276000000E+02   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        -0.402838545E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441908E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
-----------------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00043664                            14
a  epsilon                  -3.105                            29
a  Local Time Step      4.2278e-08                        281648


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5432          5.0027         0.50551         0.11469
v  Velocity[Y]              -4.611          6.7911         0.37584         0.27243
v  Velocity[Z]             -7.7368          4.3953        -0.29714       -0.001543
v  ǁVelocityǁ            0.0021198          8.8021          1.8025          2.2409
v  Pressure                -2190.8           26621           17667           14347
v  k                    1.6198e-08         0.73293       0.0088165        0.012373
v  epsilon              0.00027253           23607          41.432          7.4419
v  TurbVisc             1.0818e-13         0.16883      0.00070173       0.0087774
v  CourantNb              0.039333           40719          105.85          24.601
v  FourierNb               0.22315      2.3653e+06          217.56           2.802
v  total_pressure       4.9781e+05      5.2662e+05      5.1767e+05      5.1435e+05
v  Local Time Step          -----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00043664                            14
a  epsilon                  -3.105                            29
a  Local Time Step      4.2278e-08                        281648


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5432          5.0027         0.50551         0.11469
v  Velocity[Y]              -4.611          6.7911         0.37584         0.27243
v  Velocity[Z]             -7.7368          4.3953        -0.29714       -0.001543
v  ǁVelocityǁ            0.0021198          8.8021          1.8025          2.2409
v  Pressure                -2190.8           26621           17667           14347
v  k                    1.6198e-08         0.73293       0.0088165        0.012373
v  epsilon              0.00027253           23607          41.432          7.4419
v  TurbVisc             1.0818e-13         0.16883      0.00070173       0.0087774
v  CourantNb              0.039333           40719          105.85          24.601
v  FourierNb               0.22315      2.3653e+06          217.56           2.802
v  total_pressure       4.9781e+05      5.2662e+05      5.1767e+05      5.1435e+05
v  Local Time Step            0.01         0.15767        0.010005        0.010046


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6744      2.3779e+06          323.41          27.403


 TIME FOR THE TIME STEP              276:        0.14364E+03

===============================================================


 INSTANT    0.277000000E+02   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        -0.103978437E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441863E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24319E+01 0.18960E+01
   Friction velocity        uet   :  0.18596E-01 0.13564E+02
   Friction velocity        uk    :  0.18245E-01 0.13564E+02
   Dimensionless distance   yplus :  0.14784E-02 0.10324E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3891
   Nb of faces within the viscous sub-layer     :      24462
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68039E+00     349   0.18995E+00   0.20591E+00 0.19352E+01 
c  Velocity[X]                                      0.57595E-01 
c  Velocity[Y]                                      0.78035E-01 
c  Velocity[Z]                                      0.70275E-01 
c  Pressure     0.22493E-01     921   0.91963E-02   0.30373E-01 0.38756E-01 
c  k            0.26738E-01     127   0.17607E-03   0.16714E-04 0.17349E+01 
c  epsilon      0.23238E+03     106   0.28611E-03   0.15822E+04 0.65732E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00044954                            23
a  epsilon                  -18.63                            35
a  Local Time Step      4.2278e-08                        281649


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5425          4.9918         0.50504         0.11463
v  Velocity[Y]             -4.6105          6.7185         0.37514          0.2725
v  Velocity[Z]             -7.7514          4.3846        -0.29783      -0.0014517
v  ǁVelocityǁ            0.0015694          8.8073          1.8028          2.2412
v  Pressure                -2194.2           26612           17660           14341
v  k                    1.6754e-08         0.72738       0.0087997        0.012375
v  epsilon              3.6098e-05           23353          41.064          7.4418
v  TurbVisc             1.0227e-13         0.16883      0.00070252       0.0087774
v  CourantNb              0.043303           41073          105.85          24.601
v  FourierNb               0.22314      2.3653e+06          217.56          2.8024
v  total_pressure       4.9781e+05      5.2661e+0------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24387E+01 0.19057E+01
   Friction velocity        uet   :  0.93361E-02 0.12839E+02
   Friction velocity        uk    :  0.95689E-02 0.12839E+02
   Dimensionless distance   yplus :  0.15094E-02 0.10329E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3872
   Nb of faces within the viscous sub-layer     :      24455
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68062E+00     360   0.19308E+00   0.21107E+00 0.19592E+01 
c  Velocity[X]                                      0.59513E-01 
c  Velocity[Y]                                      0.78253E-01 
c  Velocity[Z]                                      0.73299E-01 
c  Pressure     0.23039E-01     866   0.94760E-02   0.31100E-01 0.26935E-01 
c  k            0.26723E-01     126   0.22947E-03   0.17319E-04 0.17673E+01 
c  epsilon      0.22943E+03     114   0.47039E-03   0.15475E+04 0.64905E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00042363                            15
a  epsilon                 -3.1791                            34
a  Local Time Step      4.2278e-08                        281649


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5498          5.0041         0.50516         0.11461
v  Velocity[Y]             -4.6051          6.7938         0.37535         0.27248
v  Velocity[Z]             -7.7625          4.3991        -0.29855      -0.0015423
v  ǁVelocityǁ            0.0022618          8.8341          1.8034           2.241
v  Pressure                -2193.6           26616           17665           14344
v  k                    1.6071e-08         0.73187       0.0088242        0.012375
v  epsilon              9.2749e-05           23561          41.479          7.4418
v  TurbVisc              1.071e-13         0.16883      0.00070191       0.0087771
v  CourantNb              0.011281           41813          105.83          24.604
v  FourierNb               0.22313      2.3653e+06          217.56          2.8024
v  total_pressure       4.9781e+05      5.2662e+05      5.1766e+05      5.1434e+05
v  Local Time Step            0.01         0.15768        0.010005        0.010046


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6726      2.3795e+06          323.39          27.407


 TIME FOR THE TIME STEP              278:        0.14876E+03

===============================================================


 INSTANT    0.279000000E+02   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        -0.773705697E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441246E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24502E+01 0.19003E+01
   Friction velocity        uet   :  0.19230E-01 0.11691E+02
   Friction velocity        uk    :  0.19188E-01 0.11691E+02
   Dimensionless distance   yplus :  0.14225E-02 0.10304E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3888
   Nb of faces within the viscous sub-layer     :      24457
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68087E+00     374   0.19312E+00   0.21475E+00 0.19762E+01 
c  Velocity[X]                                      0.61356E-01 
c  Velocity[Y]                                      0.78853E-01 
c  Velocity[Z]                                      0.74538E-01 
c  Pressure     0.23466E-01     871   0.96811E-02   0.31686E-01 0.29594E-01 
c  k            0.26744E-01     130   0.20374E-03   0.15649E-04 0.16799E+01 
c  epsilon      0.23277E+03     110   0.29519E-03   0.14338E+04 0.62394E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00044141                            25
a  epsilon                 -26.838                            39
a  Local Time Step      4.2278e-08                        281657


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5718          4.9962         0.50526         0.11457
v  Velocity[Y]             -4.6086          6.7311         0.37554         0.27241
v  Velocity[Z]             -7.7757          4.3805        -0.29758      -0.0014991
v  ǁVelocityǁ            0.0025541          8.8371          1.8032          2.2412
v  Pressure                -2196.3           26609           17659           14340
v  k                    9.7423e-09         0.73148       0.0088147        0.012378
v  epsilon              0.00010251           23556          41.192          7.4458
v  TurbVisc             1.0206e-13         0.16883       0.0007027       0.0087773
v  CourantNb              0.019619           40539          105.97          24.604
v  FourierNb               0.22313      2.3653e+06          217.56          2.8019
v  total_pressure        4.978e+05      5.2661e+05      5.1766e+05      5.1434e+05
v  Local Time Step            0.01         0.12308        0.010005        0.010043


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6825      2.3816e+06          323.54          27.406


 TIME FOR THE TIME STEP              279:        0.14911E+03

===============================================================


 INSTANT    0.280000000E+02   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        -0.856514489E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441854E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24566E+01 0.19018E+01
   Friction velocity        uet   :  0.21546E-01 0.10729E+02
   Friction velocity        uk    :  0.21058E-01 0.10729E+02
   Dimensionless distance   yplus :  0.13389E-02 0.10188E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3874
   Nb of faces within the viscous sub-layer     :      24454
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68029E+00     352   0.19108E+00   0.21731E+00 0.19881E+01 
c  Velocity[X]                                      0.65269E-01 
c  Velocity[Y]                                      0.78119E-01 
c  Velocity[Z]                                      0.73921E-01 
c  Pressure     0.23728E-01     637   0.97305E-02   0.32029E-01 0.17862E-01 
c  k            0.26723E-01     127   0.19410E-03   0.13292E-04 0.15485E+01 
c  epsilon      0.22938E+03     102   0.45328E-03   0.12381E+04 0.58213E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00042965                            13
a  epsilon                 -3.1906                            28
a  Local Time Step      4.2278e-08                        281649


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5424          4.9872         0.50505         0.11452
v  Velocity[Y]             -4.6205           6.768         0.37504         0.27248
v  Velocity[Z]             -7.7572          4.4356        -0.29781      -0.0015552
v  ǁVelocityǁ            0.0023682          8.8222          1.8025           2.241
v  Pressure                -2197.5           26609           17659           14339
v  k                    1.5995e-08         0.72888       0.0088124        0.012377
v  epsilon              0.00012865           23422          41.348          7.4363
v  TurbVisc             3.6335e-14         0.16883      0.00070214       0.0087775
v  CourantNb             0.0093292           41166          105.95          24.605
v  FourierNb               0.22312      2.3653e+06          217.56          2.8021
v  total_pressure        4.978e+05      5.2661e+05      5.1766e+05      5.1434e+05
v  Local Time Step            0.01         0.12748        0.010005        0.010044


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6975      2.3817e+06          323.51          27.407


 TIME FOR THE TIME STEP              280:        0.13381E+03

===============================================================


 INSTANT    0.281000000E+02   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        -0.668555665E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441875E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24530E+01 0.19020E+01
   Friction velocity        uet   :  0.24917E-01 0.10727E+02
   Friction velocity        uk    :  0.24889E-01 0.10727E+02
   Dimensionless distance   yplus :  0.10775E-02 0.10300E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3881
   Nb of faces within the viscous sub-layer     :      24459
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68039E+00     377   0.19095E+00   0.21107E+00 0.19592E+01 
c  Velocity[X]                                      0.59677E-01 
c  Velocity[Y]                                      0.77202E-01 
c  Velocity[Z]                                      0.74186E-01 
c  Pressure     0.22458E-01     374   0.91982E-02   0.30326E-01 0.13046E-01 
c  k            0.26739E-01     133   0.16705E-03   0.15029E-04 0.16463E+01 
c  epsilon      0.23286E+03     106   0.27484E-03   0.13668E+04 0.60991E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0004726                            24
a  epsilon                 -26.581                            35
a  Local Time Step      4.2278e-08                        281651


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5513          5.0039         0.50458          0.1146
v  Velocity[Y]             -4.6048          6.6823         0.37566         0.27254
v  Velocity[Z]             -7.7752          4.3767        -0.29897      -0.0014541
v  ǁVelocityǁ            0.0022647          8.8519          1.8033          2.2412
v  Pressure                  -2196           26609           17658           14339
v  k                     7.551e-09           0.733        0.008823        0.012379
v  epsilon              0.00024181           23621          41.163          7.4455
v  TurbVisc             1.0203e-13         0.16883      0.00070261       0.0087776
v  CourantNb              0.035078           40463          105.89          24.603
v  FourierNb               0.22311      2.3653e+06          217.57          2.8019
v  total_pressure        4.978e+05      5.2661e+05      5.1766e+05      5.1434e+05
v  Local Time Step            0.01         0.14023        0.010005        0.010045


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7034      2.3843e+06          323.46          27.405


 TIME FOR THE TIME STEP              281:        0.12687E+03

===============================================================


 INSTANT    0.282000000E+02   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        -0.965039976E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441277E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24546E+01 0.19025E+01
   Friction velocity        uet   :  0.15045E-01 0.98239E+01
   Friction velocity        uk    :  0.15028E-01 0.98239E+01
   Dimensionless distance   yplus :  0.11420E-02 0.10306E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3875
   Nb of faces within the viscous sub-layer     :      24459
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68066E+00     356   0.19534E+00   0.21011E+00 0.19546E+01 
c  Velocity[X]                                      0.58636E-01 
c  Velocity[Y]                                      0.79159E-01 
c  Velocity[Z]                                      0.72311E-01 
c  Pressure     0.22937E-01     882   0.94002E-02   0.30960E-01 0.27548E-01 
c  k            0.26727E-01     127   0.20637E-03   0.17443E-04 0.17739E+01 
c  epsilon      0.22926E+03      99   0.44412E-03   0.13112E+04 0.59852E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00044178                            13
a  epsilon                 -3.1018                            29
a  Local Time Step      4.2278e-08                        281649


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5357          4.9815         0.50531         0.11466
v  Velocity[Y]             -4.5965          6.6887         0.37635         0.27256
v  Velocity[Z]             -7.7233          4.8089        -0.29879      -0.0014837
v  ǁVelocityǁ            0.0027395          8.7861          1.8035          2.2412
v  Pressure                -2193.3           26615           17664           14343
v  k                    1.6303e-08         0.72853       0.0088099        0.012377
v  epsilon              1.8767e-05           23383          41.284           7.441
v  TurbVisc             2.1777e-14         0.16883      0.00070242       0.0087776
v  CourantNb              0.034711           40402          105.97          24.606
v  FourierNb               0.22311      2.3653e+06          217.57          2.8021
v  total_pressure       4.9781e+05      5.2662e+05      5.1766e+05      5.1434e+05
v  Local Time Step            0.01         0.14041        0.010005        0.010046


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6911      2.3842e+06          323.53          27.408


 TIME FOR THE TIME STEP              282:        0.14846E+03

===============================================================


 INSTANT    0.283000000E+02   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        -0.181659401E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441229E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24405E+01 0.18968E+01
   Friction velocity        uet   :  0.20204E-01 0.10266E+02
   Friction velocity        uk    :  0.20181E-01 0.10266E+02
   Dimensionless distance   yplus :  0.11734E-02 0.10276E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3889
   Nb of faces within the viscous sub-layer     :      24455
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68039E+00     386   0.19141E+00   0.21122E+00 0.19598E+01 
c  Velocity[X]                                      0.61986E-01 
c  Velocity[Y]                                      0.76723E-01 
c  Velocity[Z]                                      0.72513E-01 
c  Pressure     0.23219E-01     726   0.95358E-02   0.31311E-01 0.11356E-01 
c  k            0.26758E-01     129   0.17743E-03   0.15269E-04 0.16594E+01 
c  epsilon      0.23312E+03     105   0.27759E-03   0.13803E+04 0.61291E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00047208                            25
a  epsilon                 -27.107                            35
a  Local Time Step      4.2278e-08                        281654


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5212          5.0213         0.50463         0.11478
v  Velocity[Y]              -4.594          6.7146         0.37571         0.27257
v  Velocity[Z]             -7.6634          4.3924        -0.29916      -0.0014316
v  ǁVelocityǁ            0.0025179          8.7288          1.8036          2.2413
v  Pressure                -2187.8           26616           17665           14344
v  k                    1.7554e-08         0.72959       0.0088293        0.012379
v  epsilon              2.6862e-05           23456          41.214          7.4513
v  TurbVisc             1.0503e-13         0.16883      0.00070253       0.0087777
v  CourantNb               0.01564           40181          105.94          24.608
v  FourierNb               0.22311      2.3653e+06          217.57          2.8022
v  total_pressure       4.9781e+05      5.2662e+05      5.1767e+05      5.1434e+05
v  Local Time Step            0.01         0.14774        0.010005        0.010046


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6895      2.3802e+06          323.51           27.41


 TIME FOR THE TIME STEP              283:        0.14079E+03

===============================================================


 INSTANT    0.284000000E+02   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        -0.114353123E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441223E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24482E+01 0.19057E+01
   Friction velocity        uet   :  0.17235E-01 0.11964E+02
   Friction velocity        uk    :  0.17216E-01 0.11964E+02
   Dimensionless distance   yplus :  0.15267E-02 0.10297E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3882
   Nb of faces within the viscous sub-layer     :      24464
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68097E+00     355   0.19452E+00   0.20540E+00 0.19326E+01 
c  Velocity[X]                                      0.57701E-01 
c  Velocity[Y]                                      0.75213E-01 
c  Velocity[Z]                                      0.72485E-01 
c  Pressure     0.22427E-01     632   0.90994E-02   0.30255E-01 0.95742E-02 
c  k            0.26724E-01     126   0.18967E-03   0.14625E-04 0.16245E+01 
c  epsilon      0.22965E+03      97   0.44721E-03   0.12639E+04 0.58686E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00043529                            14
a  epsilon                 -3.2519                            28
a  Local Time Step      4.2278e-08                        281652


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5173          5.0275         0.50474         0.11481
v  Velocity[Y]             -4.6027           6.704         0.37568         0.27257
v  Velocity[Z]             -7.6932          4.5181        -0.29949      -0.0014899
v  ǁVelocityǁ            0.0023588          8.7654          1.8038          2.2411
v  Pressure                -2182.6           26617           17666           14344
v  k                     1.643e-08         0.73151       0.0088147        0.012375
v  epsilon              8.6165e-05           23535          41.416           7.439
v  TurbVisc             1.1372e-13         0.16883      0.00070193       0.0087776
v  CourantNb              0.064798           40893          105.97          24.609
v  FourierNb               0.22313      2.3653e+06          217.57          2.8023
v  total_pressure       4.9782e+05      5.2662e+05      5.1767e+05      5.1434e+05
v  Local Time Step            0.01         0.15653        0.010005        0.010046


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6629       2.382e+06          323.54          27.411


 TIME FOR THE TIME STEP              284:        0.13469E+03

===============================================================


 INSTANT    0.285000000E+02   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        -0.172042078E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441256E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24431E+01 0.18989E+01
   Friction velocity        uet   :  0.21212E-01 0.12628E+02
   Friction velocity        uk    :  0.21205E-01 0.12628E+02
   Dimensionless distance   yplus :  0.16113E-02 0.10279E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3896
   Nb of faces within the viscous sub-layer     :      24464
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68059E+00     381   0.19261E+00   0.20991E+00 0.19539E+01 
c  Velocity[X]                                      0.57783E-01 
c  Velocity[Y]                                      0.76637E-01 
c  Velocity[Z]                                      0.75491E-01 
c  Pressure     0.22505E-01     790   0.90640E-02   0.30363E-01 0.14925E-01 
c  k            0.26749E-01     130   0.16306E-03   0.13540E-04 0.15626E+01 
c  epsilon      0.23241E+03     104   0.27630E-03   0.12405E+04 0.58085E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00046091                            13
a  epsilon                 -27.129                            21
a  Local Time Step      4.2278e-08                        281649


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5258          5.0049         0.50466         0.11475
v  Velocity[Y]             -4.5967          6.7191         0.37617         0.27256
v  Velocity[Z]             -7.7677          4.3778        -0.29867      -0.0014668
v  ǁVelocityǁ            0.0026093          8.8341          1.8041           2.241
v  Pressure                -2176.2           26620           17668           14346
v  k                    1.4052e-08         0.73026       0.0088073        0.012375
v  epsilon              6.4877e-05           23490          41.117          7.4459
v  TurbVisc             9.9982e-14         0.16883      0.00070185       0.0087774
v  CourantNb             0.0082808           41740          105.92          24.606
v  FourierNb               0.22313      2.3653e+06          217.57          2.8026
v  total_pressure       4.9782e+05      5.2662e+05      5.1767e+05      5.1435e+05
v  Local Time Step            0.01         0.16355        0.010005        0.010046


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.661       2.377e+06          323.49          27.409


 TIME FOR THE TIME STEP              285:        0.14641E+03

===============================================================


 INSTANT    0.286000000E+02   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        -0.545910046E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441264E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24357E+01 0.19014E+01
   Friction velocity        uet   :  0.15263E-01 0.11624E+02
   Friction velocity        uk    :  0.15261E-01 0.11624E+02
   Dimensionless distance   yplus :  0.14832E-02 0.10309E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3877
   Nb of faces within the viscous sub-layer     :      24464
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68058E+00     363   0.18920E+00   0.20951E+00 0.19519E+01 
c  Velocity[X]                                      0.59338E-01 
c  Velocity[Y]                                      0.76011E-01 
c  Velocity[Z]                                      0.74164E-01 
c  Pressure     0.22717E-01     790   0.91959E-02   0.30650E-01 0.15718E-01 
c  k            0.26729E-01     126   0.17999E-03   0.16670E-04 0.17342E+01 
c  epsilon      0.22980E+03      95   0.40844E-03   0.31193E+04 0.92099E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.000442                            26
a  epsilon                 -3.1457                            45
a  Local Time Step      4.2278e-08                        281653


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5663          4.9905         0.50523         0.11469
v  Velocity[Y]             -4.6204           6.716         0.37554         0.27252
v  Velocity[Z]             -7.7228          4.4152        -0.29822       -0.001512
v  ǁVelocityǁ            0.0025806          8.7766          1.8034          2.2411
v  Pressure                -2168.4           26624           17671           14347
v  k                    1.3165e-08         0.72887       0.0088152        0.012374
v  epsilon              8.4638e-05           23413          41.347          7.4435
v  TurbVisc             7.7438e-14         0.16883      0.00070114       0.0087771
v  CourantNb              0.029485           42323          105.95          24.604
v  FourierNb               0.22314      2.3653e+06          217.56          2.8023
v  total_pressure       4.9783e+05      5.2662e+05      5.1767e+05      5.1435e+05
v  Local Time Step            0.01         0.16022        0.010005        0.010046


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6571      2.3778e+06          323.52          27.406


 TIME FOR THE TIME STEP              286:        0.14459E+03

===============================================================


 INSTANT    0.287000000E+02   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        -0.159764609E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441245E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24341E+01 0.19011E+01
   Friction velocity        uet   :  0.12009E-01 0.10501E+02
   Friction velocity        uk    :  0.11893E-01 0.10501E+02
   Dimensionless distance   yplus :  0.13226E-02 0.10142E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3891
   Nb of faces within the viscous sub-layer     :      24457
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68077E+00     382   0.19394E+00   0.20269E+00 0.19200E+01 
c  Velocity[X]                                      0.59533E-01 
c  Velocity[Y]                                      0.74998E-01 
c  Velocity[Z]                                      0.68161E-01 
c  Pressure     0.22725E-01     776   0.93097E-02   0.30658E-01 0.17289E-01 
c  k            0.26736E-01     133   0.16754E-03   0.16684E-04 0.17347E+01 
c  epsilon      0.23223E+03     104   0.29094E-03   0.31009E+04 0.91815E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00046751                            13
a  epsilon                 -1.1125                            21
a  Local Time Step      4.2278e-08                        281651


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5287          5.0205         0.50518         0.11471
v  Velocity[Y]             -4.6191          6.7008         0.37556         0.27254
v  Velocity[Z]             -7.7386          4.3735        -0.29869      -0.0015071
v  ǁVelocityǁ            0.0031958          8.8067          1.8036          2.2411
v  Pressure                -2161.1           26622           17667           14346
v  k                    2.6195e-09         0.73226       0.0088029        0.012376
v  epsilon              5.0742e-05           23609          41.117          7.4443
v  TurbVisc             8.3407e-14         0.16883       0.0007014       0.0087773
v  CourantNb              0.013739           42027          105.88          24.604
v  FourierNb               0.22315      2.3653e+06          217.56          2.8014
v  total_pressure       4.9784e+05      5.2662e+05      5.1767e+05      5.1435e+05
v  Local Time Step            0.01         0.16242        0.010005        0.010047


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6527      2.3829e+06          323.44          27.405


 TIME FOR THE TIME STEP              287:        0.14118E+03

===============================================================


 INSTANT    0.288000000E+02   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        -0.941754845E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441852E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24418E+01 0.19044E+01
   Friction velocity        uet   :  0.16555E-01 0.12840E+02
   Friction velocity        uk    :  0.16550E-01 0.12840E+02
   Dimensionless distance   yplus :  0.16384E-02 0.10327E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3877
   Nb of faces within the viscous sub-layer     :      24453
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68062E+00     356   0.19934E+00   0.21224E+00 0.19646E+01 
c  Velocity[X]                                      0.60082E-01 
c  Velocity[Y]                                      0.76851E-01 
c  Velocity[Z]                                      0.75305E-01 
c  Pressure     0.23098E-01     761   0.93416E-02   0.31163E-01 0.15095E-01 
c  k            0.26728E-01     128   0.21972E-03   0.13992E-04 0.15887E+01 
c  epsilon      0.22925E+03     102   0.57604E-03   0.14287E+04 0.62444E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0004288                            13
a  epsilon                 -3.0519                            27
a  Local Time Step      4.2278e-08                        281650


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5117           5.004         0.50537          0.1147
v  Velocity[Y]             -4.6062          6.7165         0.37625         0.27258
v  Velocity[Z]             -7.7319          4.4032        -0.29859      -0.0015722
v  ǁVelocityǁ            0.0033598          8.7807          1.8041          2.2411
v  Pressure                -2157.1           26618           17665           14344
v  k                    1.0745e-08         0.73026       0.0088207        0.012376
v  epsilon              8.5663e-05           23499          41.725          7.4423
v  TurbVisc             2.4525e-15         0.16883      0.00070066       0.0087775
v  CourantNb              0.068657           42380          105.91          24.602
v  FourierNb               0.22316      2.3653e+06          217.56          2.8022
v  total_pressure       4.9784e+05      5.2662e+05      5.1766e+05      5.1434e+05
v  Local Time Step            0.01         0.16355        0.010006        0.010049


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6538      2.3804e+06          323.47          27.405


 TIME FOR THE TIME STEP              288:        0.13574E+03

===============================================================


 INSTANT    0.289000000E+02   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        -0.853671249E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441849E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24508E+01 0.19004E+01
   Friction velocity        uet   :  0.77460E-02 0.11278E+02
   Friction velocity        uk    :  0.77094E-02 0.11278E+02
   Dimensionless distance   yplus :  0.14391E-02 0.10305E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3891
   Nb of faces within the viscous sub-layer     :      24454
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68056E+00     382   0.19510E+00   0.22328E+00 0.20151E+01 
c  Velocity[X]                                      0.64741E-01 
c  Velocity[Y]                                      0.80728E-01 
c  Velocity[Z]                                      0.77810E-01 
c  Pressure     0.23678E-01     730   0.95362E-02   0.31951E-01 0.12067E-01 
c  k            0.26742E-01     132   0.17132E-03   0.15897E-04 0.16933E+01 
c  epsilon      0.23267E+03     110   0.33462E-03   0.13450E+04 0.60559E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00045159                            36
a  epsilon                 -40.455                            56
a  Local Time Step      4.2278e-08                        281651


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5559          4.9897         0.50487         0.11469
v  Velocity[Y]             -4.6079          6.7248         0.37552         0.27262
v  Velocity[Z]             -7.7334          4.8573        -0.29836      -0.0015024
v  ǁVelocityǁ             0.002942           8.787          1.8029          2.2412
v  Pressure                -2159.1           26617           17663           14342
v  k                    1.1211e-08         0.73076        0.008802        0.012377
v  epsilon               4.375e-05           23534          41.095          7.4445
v  TurbVisc             6.4466e-14         0.16883      0.00070141       0.0087777
v  CourantNb             0.0067097           42015          105.94          24.606
v  FourierNb               0.22316      2.3653e+06          217.56          2.8019
v  total_pressure       4.9784e+05      5.2662e+05      5.1766e+05      5.1434e+05
v  Local Time Step            0.01         0.13102        0.010005        0.010047


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6486      2.3816e+06           323.5          27.408


 TIME FOR THE TIME STEP              289:        0.13734E+03

===============================================================


 INSTANT    0.290000000E+02   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        -0.466273127E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441870E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24495E+01 0.19072E+01
   Friction velocity        uet   :  0.20232E-01 0.10059E+02
   Friction velocity        uk    :  0.19959E-01 0.10059E+02
   Dimensionless distance   yplus :  0.12008E-02 0.10320E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3875
   Nb of faces within the viscous sub-layer     :      24458
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68061E+00     371   0.19376E+00   0.21658E+00 0.19847E+01 
c  Velocity[X]                                      0.61398E-01 
c  Velocity[Y]                                      0.79766E-01 
c  Velocity[Z]                                      0.75417E-01 
c  Pressure     0.22977E-01     868   0.92960E-02   0.31006E-01 0.25025E-01 
c  k            0.26715E-01     128   0.18466E-03   0.15521E-04 0.16735E+01 
c  epsilon      0.22937E+03     104   0.38073E-03   0.13526E+04 0.60734E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00047998                            14
a  epsilon                 -3.1312                            31
a  Local Time Step      4.2278e-08                        281647


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5641           4.996         0.50471         0.11469
v  Velocity[Y]             -4.6022          6.7476         0.37624          0.2726
v  Velocity[Z]             -7.6986          4.4134        -0.29874      -0.0015575
v  ǁVelocityǁ            0.0027773          8.7572          1.8034          2.2411
v  Pressure                -2154.5           26625           17667           14346
v  k                    1.0937e-08         0.73201       0.0088006        0.012373
v  epsilon              0.00011841           23558          41.194          7.4374
v  TurbVisc             7.2405e-14         0.16883      0.00070054       0.0087773
v  CourantNb                0.0423           43158          105.83          24.604
v  FourierNb               0.22315      2.3653e+06          217.56          2.8019
v  total_pressure       4.9785e+05      5.2662e+05      5.1767e+05      5.1435e+05
v  Local Time Step            0.01         0.14412        0.010005        0.010047


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6525      2.3819e+06          323.39          27.406


 TIME FOR THE TIME STEP              290:        0.14157E+03

===============================================================


 INSTANT    0.291000000E+02   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        -0.666148794E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441249E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24518E+01 0.18988E+01
   Friction velocity        uet   :  0.27875E-01 0.10932E+02
   Friction velocity        uk    :  0.26931E-01 0.10932E+02
   Dimensionless distance   yplus :  0.13949E-02 0.10290E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3899
   Nb of faces within the viscous sub-layer     :      24458
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68076E+00     362   0.18967E+00   0.21224E+00 0.19647E+01 
c  Velocity[X]                                      0.59082E-01 
c  Velocity[Y]                                      0.78839E-01 
c  Velocity[Z]                                      0.74320E-01 
c  Pressure     0.22817E-01     755   0.91566E-02   0.30781E-01 0.13381E-01 
c  k            0.26741E-01     130   0.16528E-03   0.13211E-04 0.15425E+01 
c  epsilon      0.23236E+03     104   0.24480E-03   0.10009E+04 0.52303E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00046721                            24
a  epsilon                -0.60406                            28
a  Local Time Step      4.2278e-08                        281650


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.4919          4.9934          0.5046         0.11483
v  Velocity[Y]             -4.6103          6.7483         0.37617         0.27255
v  Velocity[Z]             -7.7796          4.3859        -0.29825      -0.0014998
v  ǁVelocityǁ            0.0022437          8.8594          1.8037          2.2411
v  Pressure                -2154.5           26622           17665           14345
v  k                    9.6717e-09         0.72933       0.0087895        0.012374
v  epsilon              1.0114e-05           23453          40.962          7.4401
v  TurbVisc             6.7657e-14         0.16883      0.00070082       0.0087769
v  CourantNb              0.013609           43113           105.9          24.605
v  FourierNb               0.22315      2.3653e+06          217.56          2.8016
v  total_pressure       4.9785e+05      5.2662e+05      5.1767e+05      5.1435e+05
v  Local Time Step            0.01         0.11444        0.010005        0.010044


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.648      2.3787e+06          323.46          27.407


 TIME FOR THE TIME STEP              291:        0.13845E+03

===============================================================


 INSTANT    0.292000000E+02   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        -0.516035600E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441840E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24499E+01 0.19031E+01
   Friction velocity        uet   :  0.18461E-01 0.10978E+02
   Friction velocity        uk    :  0.18440E-01 0.10978E+02
   Dimensionless distance   yplus :  0.14008E-02 0.10283E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3876
   Nb of faces within the viscous sub-layer     :      24451
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68038E+00     376   0.19504E+00   0.20374E+00 0.19249E+01 
c  Velocity[X]                                      0.57335E-01 
c  Velocity[Y]                                      0.74585E-01 
c  Velocity[Z]                                      0.71816E-01 
c  Pressure     0.22551E-01     724   0.90742E-02   0.30426E-01 0.14193E-01 
c  k            0.26722E-01     129   0.20229E-03   0.13959E-04 0.15870E+01 
c  epsilon      0.22959E+03      95   0.56151E-03   0.12185E+04 0.57672E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00045904                            14
a  epsilon                 -3.2896                            29
a  Local Time Step      4.2278e-08                        281658


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5874          4.9847         0.50447         0.11481
v  Velocity[Y]             -4.5996          6.7205          0.3757         0.27252
v  Velocity[Z]             -7.7474          4.4087        -0.29845      -0.0014921
v  ǁVelocityǁ            0.0015844          8.8168          1.8035           2.241
v  Pressure                -2155.1           26620           17663           14343
v  k                    9.6023e-09         0.73105       0.0088179        0.012372
v  epsilon              0.00014174           23513          41.678          7.4401
v  TurbVisc              5.877e-14         0.16883      0.00070061       0.0087767
v  CourantNb            0.00070264           42929          105.93          24.606
v  FourierNb               0.22313      2.3653e+06          217.56          2.8016
v  total_pressure       4.9784e+05      5.2662e+05      5.1766e+05      5.1434e+05
v  Local Time Step            0.01         0.12589        0.010005        0.010045


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6576      2.3814e+06          323.49          27.408


 TIME FOR THE TIME STEP              292:        0.13644E+03

===============================================================


 INSTANT    0.293000000E+02   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        -0.755783757E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441829E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24478E+01 0.18981E+01
   Friction velocity        uet   :  0.21004E-01 0.10089E+02
   Friction velocity        uk    :  0.20959E-01 0.10089E+02
   Dimensionless distance   yplus :  0.12873E-02 0.10279E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3882
   Nb of faces within the viscous sub-layer     :      24452
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68011E+00     368   0.19410E+00   0.21699E+00 0.19865E+01 
c  Velocity[X]                                      0.62716E-01 
c  Velocity[Y]                                      0.79729E-01 
c  Velocity[Z]                                      0.74547E-01 
c  Pressure     0.22889E-01     868   0.93418E-02   0.30871E-01 0.28090E-01 
c  k            0.26738E-01     132   0.17112E-03   0.14775E-04 0.16326E+01 
c  epsilon      0.23276E+03     106   0.33686E-03   0.16740E+04 0.67535E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00045286                            36
a  epsilon                 -39.545                            58
a  Local Time Step      4.2278e-08                        281643


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5296          4.9757         0.50428          0.1148
v  Velocity[Y]             -4.5864          6.7503         0.37556         0.27264
v  Velocity[Z]              -7.737          4.3898        -0.29891      -0.0014713
v  ǁVelocityǁ            0.0018531          8.7911          1.8034          2.2413
v  Pressure                -2155.6           26626           17669           14347
v  k                    7.9078e-09         0.72819       0.0087951        0.012372
v  epsilon              1.9328e-05           23415          41.116          7.4408
v  TurbVisc             6.1315e-14         0.16883      0.00070108       0.0087765
v  CourantNb              0.008319           42493          105.93          24.603
v  FourierNb               0.22313      2.3653e+06          217.56          2.8019
v  total_pressure       4.9784e+05      5.2663e+05      5.1767e+05      5.1435e+05
v  Local Time Step            0.01         0.13022        0.010005        0.010045


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6562      2.3797e+06          323.49          27.405


 TIME FOR THE TIME STEP              293:        0.14537E+03

===============================================================


 INSTANT    0.294000000E+02   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        -0.443293533E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441227E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24473E+01 0.19059E+01
   Friction velocity        uet   :  0.19356E-01 0.65125E+01
   Friction velocity        uk    :  0.19313E-01 0.65125E+01
   Dimensionless distance   yplus :  0.72321E-03 0.10293E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3882
   Nb of faces within the viscous sub-layer     :      24467
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68042E+00     385   0.19143E+00   0.21491E+00 0.19766E+01 
c  Velocity[X]                                      0.65548E-01 
c  Velocity[Y]                                      0.77812E-01 
c  Velocity[Z]                                      0.71549E-01 
c  Pressure     0.22880E-01     716   0.92349E-02   0.30854E-01 0.12613E-01 
c  k            0.26720E-01     125   0.19866E-03   0.15862E-04 0.16917E+01 
c  epsilon      0.22966E+03     114   0.42687E-03   0.13091E+04 0.59761E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00045765                            15
a  epsilon                  -2.865                            31
a  Local Time Step      4.2278e-08                        281647


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5688          4.9967         0.50474         0.11482
v  Velocity[Y]             -4.5968          6.7582         0.37662         0.27271
v  Velocity[Z]             -7.7488          4.3903         -0.2991      -0.0014671
v  ǁVelocityǁ            0.0013048          8.8208          1.8046          2.2414
v  Pressure                -2160.2           26625           17668           14346
v  k                    6.5735e-09         0.73279        0.008796         0.01237
v  epsilon              0.00012345           23632          41.223          7.4376
v  TurbVisc             4.3889e-14         0.16883      0.00070058       0.0087764
v  CourantNb               0.06663           42868           105.9          24.606
v  FourierNb               0.22312      2.3653e+06          217.56          2.8021
v  total_pressure       4.9784e+05      5.2662e+05      5.1767e+05      5.1435e+05
v  Local Time Step            0.01         0.14126        0.010005        0.010045


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6557      2.3802e+06          323.46          27.409


 TIME FOR THE TIME STEP              294:        0.13783E+03

===============================================================


 INSTANT    0.295000000E+02   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        -0.762252990E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441820E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24512E+01 0.19054E+01
   Friction velocity        uet   :  0.21228E-01 0.65934E+01
   Friction velocity        uk    :  0.21115E-01 0.65934E+01
   Dimensionless distance   yplus :  0.72038E-03 0.10264E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3884
   Nb of faces within the viscous sub-layer     :      24463
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68069E+00     360   0.19317E+00   0.21104E+00 0.19589E+01 
c  Velocity[X]                                      0.61905E-01 
c  Velocity[Y]                                      0.77971E-01 
c  Velocity[Z]                                      0.71165E-01 
c  Pressure     0.22636E-01     718   0.91954E-02   0.30518E-01 0.11238E-01 
c  k            0.26741E-01     144   0.16939E-03   0.13945E-04 0.15862E+01 
c  epsilon      0.23284E+03     114   0.26065E-03   0.11655E+04 0.56351E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00044699                            23
a  epsilon                 -19.038                            33
a  Local Time Step      4.2278e-08                        281656


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5526          4.9889         0.50407         0.11488
v  Velocity[Y]             -4.5996          6.7636         0.37595          0.2727
v  Velocity[Z]             -7.7329          4.3901        -0.29826      -0.0014323
v  ǁVelocityǁ            0.0030955          8.8135          1.8028          2.2411
v  Pressure                -2157.6           26627           17669           14347
v  k                    1.0198e-08         0.73356       0.0088049         0.01237
v  epsilon              3.0379e-05           23686          41.119          7.4397
v  TurbVisc             4.1443e-14         0.16883      0.00070124       0.0087763
v  CourantNb              0.010963           43165          105.97           24.61
v  FourierNb               0.22312      2.3653e+06          217.56          2.8022
v  total_pressure       4.9784e+05      5.2663e+05      5.1767e+05      5.1435e+05
v  Local Time Step            0.01         0.13382        0.010005        0.010044


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6643      2.3776e+06          323.53          27.413


 TIME FOR THE TIME STEP              295:        0.13668E+03

===============================================================


 INSTANT    0.296000000E+02   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        -0.661133207E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441246E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24495E+01 0.19075E+01
   Friction velocity        uet   :  0.12686E-01 0.84613E+01
   Friction velocity        uk    :  0.12556E-01 0.84613E+01
   Dimensionless distance   yplus :  0.62552E-03 0.10107E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3881
   Nb of faces within the viscous sub-layer     :      24455
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68045E+00     362   0.18980E+00   0.21122E+00 0.19596E+01 
c  Velocity[X]                                      0.61716E-01 
c  Velocity[Y]                                      0.76744E-01 
c  Velocity[Z]                                      0.72755E-01 
c  Pressure     0.22611E-01     562   0.91825E-02   0.30502E-01 0.99280E-02 
c  k            0.26724E-01     130   0.20680E-03   0.16231E-04 0.17112E+01 
c  epsilon      0.22994E+03     104   0.45644E-03   0.13860E+04 0.61454E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00042826                            17
a  epsilon                 -3.2564                            25
a  Local Time Step      4.2278e-08                        281646


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5487            4.99         0.50451           0.115
v  Velocity[Y]             -4.5945          6.7374         0.37598         0.27267
v  Velocity[Z]             -7.6193          4.4009        -0.29877      -0.0014379
v  ǁVelocityǁ            0.0035007          8.7076          1.8031          2.2412
v  Pressure                -2153.1           26627           17670           14347
v  k                    8.6515e-09         0.73026       0.0088059        0.012371
v  epsilon              3.1823e-05           23493          41.405          7.4385
v  TurbVisc             3.5909e-14         0.16883      0.00070064       0.0087762
v  CourantNb              0.028928           44041          105.76          24.605
v  FourierNb               0.22312      2.3653e+06          217.56          2.8019
v  total_pressure       4.9785e+05      5.2663e+05      5.1767e+05      5.1435e+05
v  Local Time Step            0.01         0.13187        0.010005        0.010045


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6304      2.3805e+06          323.32          27.407


 TIME FOR THE TIME STEP              296:        0.12992E+03

===============================================================


 INSTANT    0.297000000E+02   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        -0.754274356E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441236E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24477E+01 0.18995E+01
   Friction velocity        uet   :  0.21373E-01 0.95375E+01
   Friction velocity        uk    :  0.21292E-01 0.95375E+01
   Dimensionless distance   yplus :  0.11525E-02 0.10250E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3887
   Nb of faces within the viscous sub-layer     :      24458
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68065E+00     355   0.19336E+00   0.21058E+00 0.19567E+01 
c  Velocity[X]                                      0.61090E-01 
c  Velocity[Y]                                      0.75658E-01 
c  Velocity[Z]                                      0.73832E-01 
c  Pressure     0.22240E-01     780   0.89879E-02   0.29991E-01 0.15509E-01 
c  k            0.26743E-01     129   0.15809E-03   0.14421E-04 0.16131E+01 
c  epsilon      0.23310E+03     111   0.27321E-03   0.12090E+04 0.57444E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00043563                            25
a  epsilon                 -27.253                            40
a  Local Time Step      4.2278e-08                        281650


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5104          4.9751         0.50416         0.11503
v  Velocity[Y]             -4.6071          6.7927         0.37616         0.27265
v  Velocity[Z]             -7.7449          4.3948        -0.29886      -0.0014147
v  ǁVelocityǁ             0.003002          8.8122          1.8038          2.2412
v  Pressure                -2147.4           26629           17672           14349
v  k                    6.5071e-09         0.72964       0.0087943         0.01237
v  epsilon              9.8202e-05           23494          41.052          7.4378
v  TurbVisc             4.2154e-14         0.16883      0.00070084       0.0087764
v  CourantNb             0.0012462           42733           105.9          24.607
v  FourierNb               0.22312      2.3653e+06          217.56          2.8016
v  total_pressure       4.9785e+05      5.2663e+05      5.1767e+05      5.1435e+05
v  Local Time Step            0.01         0.13698        0.010005        0.010044


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6482      2.3804e+06          323.46          27.409


 TIME FOR THE TIME STEP              297:        0.13874E+03

===============================================================


 INSTANT    0.298000000E+02   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        -0.372656580E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441216E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           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+01 0.19087E+01
   Friction velocity        uet   :  0.21143E-01 0.86211E+01
   Friction velocity        uk    :  0.20854E-01 0.86211E+01
   Dimensionless distance   yplus :  0.72623E-03 0.10278E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3884
   Nb of faces within the viscous sub-layer     :      24463
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68119E+00     354   0.19572E+00   0.21946E+00 0.19974E+01 
c  Velocity[X]                                      0.61986E-01 
c  Velocity[Y]                                      0.80151E-01 
c  Velocity[Z]                                      0.77319E-01 
c  Pressure     0.23165E-01     704   0.93691E-02   0.31229E-01 0.12400E-01 
c  k            0.26733E-01     129   0.17589E-03   0.14950E-04 0.16418E+01 
c  epsilon      0.22996E+03     120   0.34528E-03   0.10398E+04 0.53180E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00043347                            14
a  epsilon                 -3.1003                            32
a  Local Time Step      4.2278e-08                        281649


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -2.501           4.998          0.5044         0.11488
v  Velocity[Y]             -4.6136          6.7074         0.37623         0.27264
v  Velocity[Z]             -7.7479          4.4177        -0.29868      -0.0013746
v  ǁVelocityǁ             0.002849          8.8069          1.8036          2.2413
v  Pressure                -2146.6           26630           17674           14350
v  k                    9.3203e-09           0.734       0.0088075        0.012371
v  epsilon              6.9312e-05           23671          41.283          7.4397
v  TurbVisc             4.2334e-14         0.16883      0.00070033       0.0087763
v  CourantNb              0.098221           42782          105.97          24.607
v  FourierNb               0.22312      2.3653e+06          217.56          2.8019
v  total_pressure       4.9785e+05      5.2663e+05      5.1767e+05      5.1435e+05
v  Local Time Step            0.01         0.13548        0.010005        0.010046


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6421      2.3803e+06          323.53          27.409


 TIME FOR THE TIME STEP              298:        0.13403E+03

===============================================================


 INSTANT    0.299000000E+02   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        -0.427972175E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441255E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24342E+01 0.19023E+01
   Friction velocity        uet   :  0.17084E-01 0.73621E+01
   Friction velocity        uk    :  0.17290E-01 0.73621E+01
   Dimensionless distance   yplus :  0.84922E-03 0.10254E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3887
   Nb of faces within the viscous sub-layer     :      24462
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68078E+00     364   0.19720E+00   0.22118E+00 0.20055E+01 
c  Velocity[X]                                      0.58678E-01 
c  Velocity[Y]                                      0.88212E-01 
c  Velocity[Z]                                      0.74289E-01 
c  Pressure     0.23244E-01     864   0.94411E-02   0.31371E-01 0.27824E-01 
c  k            0.26736E-01     131   0.15715E-03   0.13321E-04 0.15504E+01 
c  epsilon      0.23284E+03     113   0.22270E-03   0.98856E+03 0.51893E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00046068                            24
a  epsilon                 -0.5988                            29
a  Local Time Step      4.2278e-08                        281649


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5564          4.9807         0.50419         0.11485
v  Velocity[Y]             -4.5948          6.7482         0.37667         0.27266
v  Velocity[Z]              -7.746          4.3838        -0.29864      -0.0013548
v  ǁVelocityǁ            0.0036021          8.8045           1.804          2.2412
v  Pressure                -2143.8           26637           17679           14354
v  k                    7.9456e-09         0.73063        0.008791        0.012371
v  epsilon              3.1059e-05           23511          41.064          7.4356
v  TurbVisc             6.1886e-14         0.16883      0.00070092       0.0087768
v  CourantNb              0.019089           42427          105.99          24.609
v  FourierNb               0.22314      2.3653e+06          217.56          2.8023
v  total_pressure       4.9786e+05      5.2664e+05      5.1768e+05      5.1435e+05
v  Local Time Step            0.01         0.12919        0.010005        0.010045


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6742      2.3825e+06          323.56          27.412


 TIME FOR THE TIME STEP              299:        0.14210E+03

===============================================================


 INSTANT    0.300000000E+02   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        -0.119111308E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441283E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24393E+01 0.19019E+01
   Friction velocity        uet   :  0.11661E-01 0.90568E+01
   Friction velocity        uk    :  0.11553E-01 0.90568E+01
   Dimensionless distance   yplus :  0.11557E-02 0.10283E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3880
   Nb of faces within the viscous sub-layer     :      24462
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68096E+00     364   0.19467E+00   0.22089E+00 0.20042E+01 
c  Velocity[X]                                      0.61486E-01 
c  Velocity[Y]                                      0.85806E-01 
c  Velocity[Z]                                      0.73598E-01 
c  Pressure     0.23141E-01     811   0.93365E-02   0.31229E-01 0.18522E-01 
c  k            0.26730E-01     144   0.22265E-03   0.15994E-04 0.16987E+01 
c  epsilon      0.22942E+03     115   0.37857E-03   0.11619E+04 0.56290E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00041889                            14
a  epsilon                 -3.2612                            27
a  Local Time Step      4.2278e-08                        281650


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5792          4.9739         0.50487         0.11493
v  Velocity[Y]             -4.5858          6.7813         0.37631         0.27272
v  Velocity[Z]             -7.7401          4.4087        -0.29804      -0.0013874
v  ǁVelocityǁ            0.0027022          8.8015          1.8045          2.2412
v  Pressure                -2140.2           26642           17683           14356
v  k                    1.1226e-08         0.72843       0.0088059        0.012372
v  epsilon              0.00011863           23400          41.228          7.4401
v  TurbVisc              4.513e-14         0.16883      0.00070009       0.0087769
v  CourantNb              0.016092           42694          105.99          24.609
v  FourierNb               0.22316      2.3653e+06          217.56          2.8021
v  total_pressure       4.9786e+05      5.2664e+05      5.1768e+05      5.1436e+05
v  Local Time Step            0.01         0.14211        0.010005        0.010045


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6701      2.3803e+06          323.56          27.411


 TIME FOR THE TIME STEP              300:        0.14913E+03

===============================================================


 INSTANT    0.301000000E+02   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        -0.108848915E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441243E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24310E+01 0.18979E+01
   Friction velocity        uet   :  0.11520E-01 0.10625E+02
   Friction velocity        uk    :  0.11460E-01 0.10625E+02
   Dimensionless distance   yplus :  0.13558E-02 0.10299E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3887
   Nb of faces within the viscous sub-layer     :      24450
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.82908E+00     455   0.16114E+00   0.82107E+02 0.28491E+02 
c  Velocity[X]                                      0.31405E+01 
c  Velocity[Y]                                      0.64184E+01 
c  Velocity[Z]                                      0.72548E+02 
c  Pressure     0.32364E-01    1928   0.35582E+00   0.43649E-01 0.53146E+02 
c  k            0.50632E-01     217   0.11526E-02   0.14198E-01 0.34752E+02 
c  epsilon      0.23300E+03     165   0.54853E-03   0.57772E+04 0.12956E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -9.699e-05                             9
a  epsilon                -0.47497                            21
a  Local Time Step      4.2278e-08                        281647


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.4914          8.4196         0.66456         0.16599
v  Velocity[Y]             -6.8286          11.998         0.57179         0.38366
v  Velocity[Z]             -11.764          6.5969        -0.33596        0.017183
v  ǁVelocityǁ            0.0060663          14.413          2.1885          3.0449
v  Pressure                 18.205           59641           36129           32398
v  k                    1.2614e-08         0.68589       0.0095027        0.016561
v  epsilon              0.00032275           22615          43.815          8.0246
v  TurbVisc             8.5822e-14         0.16883      0.00070076       0.0087772
v  CourantNb              0.021727           42361          106.08           24.61
v  FourierNb               0.22319      2.3653e+06          217.56          2.8019
v  total_pressure       5.0002e+05      5.5964e+05      5.3613e+05       5.324e+05
v  Local Time Step            0.01         0.15632        0.010005        0.010045


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6539      2.3823e+06          323.65          27.412


 TIME FOR THE TIME STEP              301:        0.20797E+03

===============================================================


 INSTANT    0.302000000E+02   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        -0.113601290E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444413E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68104E+01 0.27782E+01
   Friction velocity        uet   :  0.20684E-01 0.26141E+02
   Friction velocity        uk    :  0.20581E-01 0.26141E+02
   Dimensionless distance   yplus :  0.31323E-02 0.11825E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5087
   Nb of faces within the viscous sub-layer     :      22395
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13444E+01     614   0.19743E+00   0.26658E+02 0.14665E+02 
c  Velocity[X]                                      0.26377E+01 
c  Velocity[Y]                                      0.46787E+01 
c  Velocity[Z]                                      0.19341E+02 
c  Pressure     0.29049E+00    1624   0.19634E+00   0.37406E+00 0.49854E+01 
c  k            0.57483E-01     215   0.21854E-02   0.11653E-01 0.25705E+02 
c  epsilon      0.86555E+03     153   0.46389E-02   0.31889E+07 0.88747E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021175                            17
a  epsilon                 -0.7858                            32
a  Local Time Step      4.2278e-08                        281676


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5186          8.2676         0.68694         0.18642
v  Velocity[Y]             -6.2087          12.901          0.6663          0.4401
v  Velocity[Z]             -13.182          8.4604        -0.22794        0.087187
v  ǁVelocityǁ            0.0097835          17.089          2.2969          3.3932
v  Pressure                -18.253           57869           37921           32240
v  k                    9.6481e-09          2.3373        0.017047         0.02137
v  epsilon              6.6687e-05      2.3931e+05           195.8          14.999
v  TurbVisc             6.6656e-14         0.21434      0.00084777        0.012863
v  CourantNb               0.13156           59820          140.13          34.897
v  FourierNb               0.22345      2.3653e+06          217.58           2.853
v  total_pressure       4.9998e+05      5.5787e+05      5.3792e+05      5.3224e+05
v  Local Time Step            0.01         0.17196        0.010002        0.010017


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.92182      2.3778e+06          357.72           37.75


 TIME FOR THE TIME STEP              302:        0.21003E+03

===============================================================


 INSTANT    0.303000000E+02   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        -0.406631770E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444412E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57588E+01 0.30970E+01
   Friction velocity        uet   :  0.30275E-01 0.44860E+02
   Friction velocity        uk    :  0.30459E-01 0.44860E+02
   Dimensionless distance   yplus :  0.57241E-02 0.12549E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4993
   Nb of faces within the viscous sub-layer     :      21887
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13698E+01     610   0.17466E+00   0.50917E+01 0.62770E+01 
c  Velocity[X]                                      0.12177E+01 
c  Velocity[Y]                                      0.18074E+01 
c  Velocity[Z]                                      0.20666E+01 
c  Pressure     0.21353E+00    1694   0.22591E+00   0.25835E+00 0.13980E+02 
c  k            0.58073E-01     184   0.12191E-02   0.35113E-02 0.14785E+02 
c  epsilon      0.10094E+04     122   0.23918E-02   0.20916E+07 0.12997E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0025869                           488
a  epsilon                 -82.542                           698
a  Local Time Step      3.8963e-08                        281694


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6752          8.3405         0.70447         0.18666
v  Velocity[Y]             -5.8213          11.626         0.69561         0.44745
v  Velocity[Z]             -10.829           8.391        -0.29255        0.055135
v  ǁVelocityǁ             0.022856          14.675          2.3662          3.4697
v  Pressure                -66.231           49488           34840           27941
v  k                    8.6642e-09          1.1548        0.012195        0.020631
v  epsilon              3.4431e-05           88920          88.715          11.821
v  TurbVisc             6.4193e-14         0.21656      0.00086081        0.013055
v  CourantNb               0.07488      2.5665e+05          148.55          35.497
v  FourierNb               0.22334      2.3653e+06          217.63          2.8545
v  total_pressure       4.9993e+05      5.4949e+05      5.3484e+05      5.2794e+05
v  Local Time Step            0.01        0.032554        0.010001        0.010009


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0737      2.6219e+06          366.18          38.352


 TIME FOR THE TIME STEP              303:        0.20723E+03

===============================================================


 INSTANT    0.304000000E+02   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        -0.372840855E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444477E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57326E+01 0.29404E+01
   Friction velocity        uet   :  0.30389E-01 0.40047E+02
   Friction velocity        uk    :  0.31467E-01 0.40047E+02
   Dimensionless distance   yplus :  0.51100E-02 0.12673E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5136
   Nb of faces within the viscous sub-layer     :      21463
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13402E+01     568   0.18633E+00   0.39947E+01 0.55829E+01 
c  Velocity[X]                                      0.73223E+00 
c  Velocity[Y]                                      0.13092E+01 
c  Velocity[Z]                                      0.19533E+01 
c  Pressure     0.22892E+00    1686   0.19084E+00   0.26296E+00 0.11131E+02 
c  k            0.58010E-01     180   0.61530E-03   0.90122E-03 0.74347E+01 
c  epsilon      0.95699E+03     140   0.10070E-02   0.29169E+06 0.43868E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00062455                           178
a  epsilon                 -17.062                           359
a  Local Time Step      4.2278e-08                        281745


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.8552          8.3038          0.7052         0.18146
v  Velocity[Y]              -5.385          10.799         0.69511         0.43662
v  Velocity[Z]             -9.8862          7.8958        -0.38509       0.0054397
v  ǁVelocityǁ            0.0091758          13.426          2.4056          3.4559
v  Pressure                -1168.2           46022           31765           24741
v  k                    7.8531e-10          1.4324        0.013801        0.020911
v  epsilon              6.9433e-06      1.1219e+05          112.36          12.663
v  TurbVisc             1.1255e-14          0.2163      0.00080476        0.013319
v  CourantNb              0.069435      2.0402e+05          149.77          35.866
v  FourierNb                0.2231      2.3653e+06          217.54          2.8547
v  total_pressure       4.9883e+05      5.4602e+05      5.3176e+05      5.2474e+05
v  Local Time Step            0.01        0.035809        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.81169      2.5693e+06          367.31          38.721


 TIME FOR THE TIME STEP              304:        0.21873E+03

===============================================================


 INSTANT    0.305000000E+02   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        -0.596400874E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444488E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54043E+01 0.27297E+01
   Friction velocity        uet   :  0.24995E-01 0.39466E+02
   Friction velocity        uk    :  0.24930E-01 0.39466E+02
   Dimensionless distance   yplus :  0.50359E-02 0.12995E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5182
   Nb of faces within the viscous sub-layer     :      21327
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13075E+01     535   0.18489E+00   0.30747E+01 0.49272E+01 
c  Velocity[X]                                      0.47598E+00 
c  Velocity[Y]                                      0.10390E+01 
c  Velocity[Z]                                      0.15598E+01 
c  Pressure     0.20956E+00    1609   0.14995E+00   0.22927E+00 0.42719E+01 
c  k            0.57731E-01     174   0.44700E-03   0.55531E-03 0.58367E+01 
c  epsilon      0.86914E+03     129   0.84179E-03   0.17260E+06 0.36709E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0022857                            73
a  epsilon                 -41.564                            88
a  Local Time Step      4.2278e-08                        281731


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.9674          7.8187          0.7087         0.17834
v  Velocity[Y]             -5.2662          10.396         0.68309         0.42788
v  Velocity[Z]             -10.132          7.4437        -0.43734       -0.017754
v  ǁVelocityǁ            0.0014666          12.864          2.4464          3.4345
v  Pressure                -3774.9           45024           30290           23652
v  k                    1.3002e-09          1.1492        0.013449        0.020942
v  epsilon              4.6656e-07           78081          100.46          12.522
v  TurbVisc             4.2164e-15         0.21629      0.00082274        0.013459
v  CourantNb              0.015748      1.3756e+05          147.52          36.096
v  FourierNb               0.22287      2.3653e+06          217.56          2.8572
v  total_pressure       4.9623e+05      5.4502e+05      5.3029e+05      5.2365e+05
v  Local Time Step            0.01         0.03939        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.77923      2.5028e+06          365.08          38.953


 TIME FOR THE TIME STEP              305:        0.20341E+03

===============================================================


 INSTANT    0.306000000E+02   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        -0.379173176E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444488E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55832E+01 0.24946E+01
   Friction velocity        uet   :  0.24270E-01 0.42653E+02
   Friction velocity        uk    :  0.24216E-01 0.42653E+02
   Dimensionless distance   yplus :  0.54426E-02 0.13153E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5292
   Nb of faces within the viscous sub-layer     :      21222
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.12925E+01     547   0.19094E+00   0.23358E+01 0.43051E+01 
c  Velocity[X]                                      0.48198E+00 
c  Velocity[Y]                                      0.81385E+00 
c  Velocity[Z]                                      0.10399E+01 
c  Pressure     0.18244E+00    1352   0.12467E+00   0.19019E+00 0.24854E+01 
c  k            0.57491E-01     172   0.30832E-03   0.30851E-03 0.43433E+01 
c  epsilon      0.79355E+03     125   0.56208E-03   0.97301E+05 0.27585E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00025816                           111
a  epsilon                 -8.5772                           213
a  Local Time Step      4.2278e-08                        281737


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.9947          7.4467         0.71723         0.17881
v  Velocity[Y]             -5.3122          10.884         0.66552         0.42538
v  Velocity[Z]             -10.002          7.2159        -0.44707       -0.016739
v  ǁVelocityǁ            0.0079027          12.433          2.4871          3.4243
v  Pressure                -4459.7           45538           30444           24169
v  k                    4.2245e-09          1.0676        0.013949        0.021027
v  epsilon              1.3496e-05           79659          105.13          12.675
v  TurbVisc             2.7359e-14         0.21629      0.00083094        0.013546
v  CourantNb              0.074176      1.0776e+05          147.38          36.342
v  FourierNb               0.22277      2.3653e+06          217.56          2.8594
v  total_pressure       4.9554e+05      5.4554e+05      5.3044e+05      5.2417e+05
v  Local Time Step            0.01        0.043329        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0525      2.4146e+06          364.94          39.201


 TIME FOR THE TIME STEP              306:        0.19598E+03

===============================================================


 INSTANT    0.307000000E+02   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        -0.834875728E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444404E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54610E+01 0.24200E+01
   Friction velocity        uet   :  0.30232E-01 0.45096E+02
   Friction velocity        uk    :  0.30185E-01 0.45096E+02
   Dimensionless distance   yplus :  0.57542E-02 0.13054E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5362
   Nb of faces within the viscous sub-layer     :      21137
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.12897E+01     529   0.18570E+00   0.18147E+01 0.37907E+01 
c  Velocity[X]                                      0.43613E+00 
c  Velocity[Y]                                      0.68633E+00 
c  Velocity[Z]                                      0.69223E+00 
c  Pressure     0.16355E+00    1525   0.10687E+00   0.16290E+00 0.43622E+01 
c  k            0.57370E-01     168   0.32174E-03   0.30352E-03 0.43017E+01 
c  epsilon      0.74225E+03      98   0.63142E-03   0.10651E+06 0.28672E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0019801                            54
a  epsilon                 -3.3053                            84
a  Local Time Step      4.2278e-08                        281728


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -3.019          7.0961         0.72781         0.18073
v  Velocity[Y]              -5.565          10.771         0.64747         0.42698
v  Velocity[Z]             -10.084          6.9746         -0.4334      -0.0077295
v  ǁVelocityǁ            0.0020969          12.148          2.5202          3.4271
v  Pressure                -4173.4           47016           31536           25409
v  k                    8.1828e-09         0.92854        0.014149        0.021098
v  epsilon              2.3032e-05           79761          106.07           12.83
v  TurbVisc             7.2143e-14         0.21629      0.00084374        0.013605
v  CourantNb               0.06096      1.0491e+05           150.1          36.584
v  FourierNb               0.22274      2.3653e+06          217.58          2.8609
v  total_pressure       4.9583e+05      5.4702e+05      5.3154e+05      5.2541e+05
v  Local Time Step            0.01        0.047662        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.1936      2.3811e+06          367.69          39.445


 TIME FOR THE TIME STEP              307:        0.19537E+03

===============================================================


 INSTANT    0.308000000E+02   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        -0.990922932E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444400E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55720E+01 0.24148E+01
   Friction velocity        uet   :  0.24541E-01 0.46869E+02
   Friction velocity        uk    :  0.24401E-01 0.46869E+02
   Dimensionless distance   yplus :  0.59805E-02 0.13118E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5418
   Nb of faces within the viscous sub-layer     :      21025
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.12959E+01     523   0.19553E+00   0.14694E+01 0.33989E+01 
c  Velocity[X]                                      0.34970E+00 
c  Velocity[Y]                                      0.60903E+00 
c  Velocity[Z]                                      0.51072E+00 
c  Pressure     0.15049E+00    1538   0.92364E-01   0.14351E+00 0.42061E+01 
c  k            0.57278E-01     169   0.27896E-03   0.26426E-03 0.40084E+01 
c  epsilon      0.69652E+03     107   0.47701E-03   0.75017E+05 0.23959E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.9063e-05                            25
a  epsilon                   -3.91                            43
a  Local Time Step      4.2278e-08                        281730


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.0637          6.9399         0.73716          0.1826
v  Velocity[Y]             -5.6666          10.351         0.62882         0.42933
v  Velocity[Z]             -10.106          6.8867        -0.41551      -0.0018509
v  ǁVelocityǁ            0.0019143          12.012          2.5472          3.4384
v  Pressure                -3714.6           48713           32813           26652
v  k                    1.6287e-08         0.92958        0.014554        0.021169
v  epsilon              1.7337e-05           56514          110.42          12.984
v  TurbVisc             1.4536e-13         0.21629      0.00085669        0.013642
v  CourantNb             0.0048934      1.0337e+05          152.66           36.82
v  FourierNb               0.22272      2.3653e+06          217.61          2.8627
v  total_pressure       4.9629e+05      5.4871e+05      5.3281e+05      5.2665e+05
v  Local Time Step            0.01        0.052428        0.010001        0.010009


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2348      2.3657e+06          370.27          39.682


 TIME FOR THE TIME STEP              308:        0.19893E+03

===============================================================


 INSTANT    0.309000000E+02   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        -0.717730305E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444394E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54572E+01 0.24052E+01
   Friction velocity        uet   :  0.26037E-01 0.48395E+02
   Friction velocity        uk    :  0.25763E-01 0.48395E+02
   Dimensionless distance   yplus :  0.61752E-02 0.13028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5443
   Nb of faces within the viscous sub-layer     :      20949
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13041E+01     538   0.19127E+00   0.12927E+01 0.31739E+01 
c  Velocity[X]                                      0.30976E+00 
c  Velocity[Y]                                      0.56477E+00 
c  Velocity[Z]                                      0.41818E+00 
c  Pressure     0.13992E+00    1486   0.80270E-01   0.12797E+00 0.30314E+01 
c  k            0.57195E-01     161   0.30770E-03   0.24634E-03 0.38654E+01 
c  epsilon      0.65510E+03     109   0.58972E-03   0.68954E+05 0.22866E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.1156e-05                             3
a  epsilon                 -3.3733                            17
a  Local Time Step      4.2278e-08                        281728


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.1095          6.7036         0.74394         0.18322
v  Velocity[Y]             -5.7713           10.72         0.61532         0.43088
v  Velocity[Z]             -9.9011          6.7953        -0.40462     -0.00087677
v  ǁVelocityǁ            0.0026943          11.909          2.5735          3.4528
v  Pressure                -3466.9           50116           33805           27529
v  k                    2.5252e-08         0.88988        0.014738         0.02123
v  epsilon              3.2425e-05           45210          112.08          13.108
v  TurbVisc             1.8916e-13         0.21629      0.00086769        0.013666
v  CourantNb              0.019987      1.0095e+05          154.69           37.03
v  FourierNb               0.22273      2.3653e+06          217.64          2.8631
v  total_pressure       4.9653e+05      5.5012e+05       5.338e+05      5.2753e+05
v  Local Time Step            0.01        0.057671        0.010001        0.010009


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.1759      2.3747e+06          372.33          39.893


 TIME FOR THE TIME STEP              309:        0.19907E+03

===============================================================


 INSTANT    0.310000000E+02   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        -0.695529442E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444397E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55009E+01 0.24062E+01
   Friction velocity        uet   :  0.30090E-01 0.47679E+02
   Friction velocity        uk    :  0.34394E-01 0.47679E+02
   Dimensionless distance   yplus :  0.60839E-02 0.13049E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5494
   Nb of faces within the viscous sub-layer     :      20830
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13107E+01     539   0.19304E+00   0.13427E+01 0.32202E+01 
c  Velocity[X]                                      0.32502E+00 
c  Velocity[Y]                                      0.64379E+00 
c  Velocity[Z]                                      0.37394E+00 
c  Pressure     0.13063E+00    1446   0.71028E-01   0.11511E+00 0.18408E+01 
c  k            0.57154E-01     163   0.36021E-03   0.20689E-03 0.35383E+01 
c  epsilon      0.62000E+03     113   0.11546E-02   0.97408E+05 0.26370E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00099385                             5
a  epsilon                 -8.5122                            15
a  Local Time Step      4.2278e-08                        281739


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.2003          6.7898         0.75137         0.18307
v  Velocity[Y]             -5.9185          10.301         0.60477         0.43207
v  Velocity[Z]             -10.053           6.678        -0.40159      -0.0028841
v  ǁVelocityǁ            0.0051149          11.829           2.601          3.4673
v  Pressure                -3506.7           51078           34402           28000
v  k                    3.2728e-08          1.1098        0.015071         0.02129
v  epsilon              0.00032838           76601          117.64          13.279
v  TurbVisc             2.1394e-13         0.21629      0.00087134        0.013682
v  CourantNb              0.042702      1.0583e+05          156.17          37.225
v  FourierNb               0.22276      2.3653e+06          217.64          2.8632
v  total_pressure       4.9649e+05      5.5108e+05       5.344e+05        5.28e+05
v  Local Time Step            0.01        0.063438        0.010001        0.010009


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.3188      2.3859e+06          373.82          40.088


 TIME FOR THE TIME STEP              310:        0.19262E+03

===============================================================


 INSTANT    0.311000000E+02   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        -0.872915746E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444397E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54373E+01 0.25449E+01
   Friction velocity        uet   :  0.28948E-01 0.45669E+02
   Friction velocity        uk    :  0.34265E-01 0.45669E+02
   Dimensionless distance   yplus :  0.53171E-02 0.13002E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5541
   Nb of faces within the viscous sub-layer     :      20789
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13179E+01     532   0.19880E+00   0.13712E+01 0.32427E+01 
c  Velocity[X]                                      0.35181E+00 
c  Velocity[Y]                                      0.62956E+00 
c  Velocity[Z]                                      0.38983E+00 
c  Pressure     0.12577E+00    1355   0.64424E-01   0.10706E+00 0.11355E+01 
c  k            0.57133E-01     158   0.28288E-03   0.18071E-03 0.33041E+01 
c  epsilon      0.59606E+03     107   0.74592E-03   0.52377E+05 0.19653E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00022861                            18
a  epsilon                 -27.199                            43
a  Local Time Step      4.2278e-08                        281742


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.2682          6.8495          0.7561         0.18254
v  Velocity[Y]             -6.0532          12.208         0.59716         0.43248
v  Velocity[Z]             -10.019          6.6478        -0.40399      -0.0053657
v  ǁVelocityǁ            0.0019662          13.382          2.6237          3.4787
v  Pressure                -3723.7           51697           34729           28209
v  k                    3.3571e-08         0.91217        0.015129        0.021341
v  epsilon              0.00044313           55436          115.78          13.365
v  TurbVisc             2.1926e-13         0.21629      0.00087791        0.013691
v  CourantNb              0.088952      1.0944e+05          157.44          37.414
v  FourierNb                0.2228      2.3653e+06          217.66           2.864
v  total_pressure       4.9628e+05       5.517e+05      5.3473e+05      5.2821e+05
v  Local Time Step            0.01        0.069782        0.010001         0.01001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5528      2.3904e+06          375.11          40.278


 TIME FOR THE TIME STEP              311:        0.18733E+03

===============================================================


 INSTANT    0.312000000E+02   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        -0.641371948E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444389E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53370E+01 0.25531E+01
   Friction velocity        uet   :  0.29438E-01 0.43107E+02
   Friction velocity        uk    :  0.32453E-01 0.43107E+02
   Dimensionless distance   yplus :  0.46272E-02 0.12949E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5587
   Nb of faces within the viscous sub-layer     :      20764
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13194E+01     523   0.20041E+00   0.13382E+01 0.31954E+01 
c  Velocity[X]                                      0.35698E+00 
c  Velocity[Y]                                      0.58420E+00 
c  Velocity[Z]                                      0.39701E+00 
c  Pressure     0.12142E+00    1302   0.59281E-01   0.10031E+00 0.88204E+00 
c  k            0.57154E-01     153   0.27076E-03   0.17515E-03 0.32501E+01 
c  epsilon      0.58219E+03     111   0.61475E-03   0.54394E+05 0.19619E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.0868e-05                             2
a  epsilon                 -1.6587                            17
a  Local Time Step      4.2278e-08                        281744


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.3318          6.9366         0.76068         0.18205
v  Velocity[Y]             -6.2073          11.494         0.59466         0.43249
v  Velocity[Z]             -10.008          6.5606        -0.41023      -0.0067931
v  ǁVelocityǁ            0.0042315          12.558          2.6486          3.4868
v  Pressure                -3962.7           52161           34968           28339
v  k                    2.9894e-08         0.93237        0.015405        0.021383
v  epsilon              0.00050643           60794          119.76          13.495
v  TurbVisc             1.8955e-13         0.21629      0.00088411        0.013698
v  CourantNb               0.10077      1.0965e+05          158.28          37.571
v  FourierNb               0.22281      2.3653e+06          217.68          2.8639
v  total_pressure       4.9604e+05      5.5216e+05      5.3497e+05      5.2834e+05
v  Local Time Step            0.01         0.07676        0.010001        0.010011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5712      2.3995e+06          375.96          40.435


 TIME FOR THE TIME STEP              312:        0.18561E+03

===============================================================


 INSTANT    0.313000000E+02   TIME STEP NUMBER             313
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---- INSTANT    0.312000000E+02   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        -0.641371948E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444389E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53370E+01 0.25531E+01
   Friction velocity        uet   :  0.29438E-01 0.43107E+02
   Friction velocity        uk    :  0.32453E-01 0.43107E+02
   Dimensionless distance   yplus :  0.46272E-02 0.12949E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5587
   Nb of faces within the viscous sub-layer     :      20764
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13194E+01     523   0.20041E+00   0.13382E+01 0.31954E+01 
c  Velocity[X]                                      0.35698E+00 
c  Velocity[Y]                                      0.58420E+00 
c  Velocity[Z]                                      0.39701E+00 
c  Pressure     0.12142E+00    1302   0.59281E-01   0.10031E+00 0.88204E+00 
c  k            0.57154E-01     153   0.27076E-03   0.17515E-03 0.32501E+01 
c  epsilon      0.58219E+03     111   0.61475E-03   0.54394E+05 0.19619E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.0868e-05                             2
a  epsilon                 -1.6587                            17
a-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.2692          7.0735         0.76404         0.18203
v  Velocity[Y]             -6.3091          12.409          0.5933         0.43272
v  Velocity[Z]             -9.9093          6.5003        -0.41521      -0.0070234
v  ǁVelocityǁ            0.0022273          13.545          2.6704          3.4929
v  Pressure                -4124.8           52609           35247           28509
v  k                    2.6802e-08          1.2152        0.015628        0.021431
v  epsilon               0.0001397           86048          125.16          13.611
v  TurbVisc             1.6585e-13         0.21629      0.00088814        0.013704
v  CourantNb             0.0043881      1.1238e+05          159.48          37.719
v  FourierNb               0.22278      2.3653e+06          217.69          2.8642
v  total_pressure       4.9588e+05      5.5261e+05      5.3525e+05      5.2851e+05
v  Local Time Step            0.01        0.074923        0.010001        0.010011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7352      2.3987e+06          377.17          40.583


 TIME FOR THE TIME STEP              313:        0.18176E+03

===============================================================


 INSTANT    0.314000000E+02   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        -0.596410734E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444384E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52809E+01 0.25708E+01
   Friction velocity        uet   :  0.14915E-01 0.43989E+02
   Friction velocity        uk    :  0.14846E-01 0.43989E+02
   Dimensionless distance   yplus :  0.35952E-02 0.12972E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5685
   Nb of faces within the viscous sub-layer     :      20627
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13240E+01     512   0.20849E+00   0.11183E+01 0.29116E+01 
c  Velocity[X]                                      0.27422E+00 
c  Velocity[Y]                                      0.48209E+00 
c  Velocity[Z]                                      0.36202E+00 
c  Pressure     0.11266E+00    1339   0.51705E-01   0.88612E-01 0.99758E+00 
c  k            0.57225E-01     156   0.28949E-03   0.17488E-03 0.32412E+01 
c  epsilon      0.57014E+03     117   0.19906E-02   0.15069E+06 0.30463E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.2892e-05                             3
a  epsilon                 -22.826                            16
a  Local Time Step      4.2278e-08                        281747


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.3836          7.1557         0.76793          0.1819
v  Velocity[Y]             -6.4176          -  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.2692          7.0735         0.76404         0.18203
v  Velocity[Y]             -6.3091          12.409          0.5933         0.43272
v  Velocity[Z]             -9.9093          6.5003        -0.41521      -0.0070234
v  ǁVelocityǁ            0.0022273          13.545          2.6704          3.4929
v  Pressure                -4124.8           52609           35247           28509
v  k                    2.6802e-08          1.2152        0.015628        0.021431
v  epsilon               0.0001397           86048          125.16          13.611
v  TurbVisc             1.6585e-13         0.21629      0.00088814        0.013704
v  CourantNb             0.0043881      1.1238e+05          159.48          37.719
v  FourierNb               0.22278      2.3653e+06          217.69          2.8642
v  total_pressure       4.9588e+05      5.5261e+05      5.3525e+05      5.2851e+05
v  Local Time Step            0.01        0.074923        0.010001        0.010011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7352      2.3987e+06          377.17          40.583


 TIME FOR THE TIME STEP              313:        0.19036E+03

===============================================================


 INSTANT    0.314000000E+02   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        -0.596410734E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444384E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52809E+01 0.25708E+01
   Friction velocity        uet   :  0.14915E-01 0.43989E+02
   Friction velocity        uk    :  0.14846E-01 0.43989E+02
   Dimensionless distance   yplus :  0.35952E-02 0.12972E+02
   ----------------------------------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13269E+01     512   0.21150E+00   0.10830E+01 0.28614E+01 
c  Velocity[X]                                      0.26718E+00 
c  Velocity[Y]                                      0.45845E+00 
c  Velocity[Z]                                      0.35739E+00 
c  Pressure     0.10994E+00    1376   0.48553E-01   0.84737E-01 0.11394E+01 
c  k            0.57299E-01     156   0.26096E-03   0.14931E-03 0.29910E+01 
c  epsilon      0.57551E+03     103   0.14660E-02   0.10806E+06 0.25631E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00040883                            27
a  epsilon                 -5.8131                            59
a  Local Time Step      4.2278e-08                        281735


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.3405          7.2627         0.77098         0.18202
v  Velocity[Y]             -6.5322          12.585         0.58703         0.43332
v  Velocity[Z]             -9.7472           6.347        -0.42756      -0.0053651
v  ǁVelocityǁ            0.0043517          13.679          2.7129          3.5024
v  Pressure                  -4107           53702           36070           29105
v  k                     1.212e-08          1.4959        0.016018         0.02152
v  epsilon              0.00016769       1.031e+05          131.35          13.881
v  TurbVisc             1.0728e-13         0.21629      0.00089581        0.013713
v  CourantNb              0.095413      1.1158e+05          162.45          37.971
v  FourierNb                0.2227      2.3653e+06           217.7          2.8657
v  total_pressure       4.9589e+05       5.537e+05      5.3607e+05      5.2911e+05
v  Local Time Step            0.01        0.055265        0.010001        0.010012


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4453      2.3965e+06          380.14          40.836


 TIME FOR THE TIME STEP              315:        0.19049E+03

===============================================================


 INSTANT    0.316000000E+02   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        -0.140458247E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444388E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51314E+01 0.27235E+01
   Friction velocity        uet   :  0.30697E-01 0.42993E+02
   Friction velocity        uk    :  0.34491E-01 0.42993E+02
   Dimensionless distance   yplus :  0.50690E-02 0.12907E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5789
   Nb of faces within the viscous sub-layer     :      20490
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
  ------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13269E+01     512   0.21150E+00   0.10830E+01 0.28614E+01 
c  Velocity[X]                                      0.26718E+00 
c  Velocity[Y]                                      0.45845E+00 
c  Velocity[Z]                                      0.35739E+00 
c  Pressure     0.10994E+00    1376   0.48553E-01   0.84737E-01 0.11394E+01 
c  k            0.57299E-01     156   0.26096E-03   0.14931E-03 0.29910E+01 
c  epsilon      0.57551E+03     103   0.14660E-02   0.10806E+06 0.25631E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00040883                            27
a  epsilon                 -5.8131                            59
a  Local Time Step      4.2278e-08                        281735


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.3405          7.2627         0.77098         0.18202
v  Velocity[Y]             -6.5322          12.585         0.58703         0.43332
v  Velocity[Z]             -9.7472           6.347        -0.42756      -0.0053651
v  ǁVelocityǁ            0.0043517          13.679          2.7129          3.5024
v  Pressure                  -4107           53702           36070           29105
v  k                     1.212e-08          1.4959        0.016018         0.02152
v  epsilon              0.00016769       1.031e+05          131.35          13.881
v  TurbVisc             1.0728e-13         0.21629      0.00089581        0.013713
v  CourantNb              0.095413      1.1158e+05          162.45          37.971
v  FourierNb                0.2227      2.3653e+06           217.7          2.8657
v  total_pressure       4.9589e+05       5.537e+05      5.3607e+05      5.2911e+05
v  Local Time Step            0.01        0.055265        0.010001        0.010012


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4453      2.3965e+06          380.14          40.836


 TIME FOR THE TIME STEP              315:        0.19424E+03

===============================================================


 INSTANT    0.316000000E+02   TIME STEP NUMBER             3Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.122623847E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444389E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54725E+01 0.27511E+01
   Friction velocity        uet   :  0.31607E-01 0.41992E+02
   Friction velocity        uk    :  0.31676E-01 0.41992E+02
   Dimensionless distance   yplus :  0.53582E-02 0.12911E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5831
   Nb of faces within the viscous sub-layer     :      20421
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13315E+01     507   0.21581E+00   0.92557E+00 0.26395E+01 
c  Velocity[X]                                      0.23829E+00 
c  Velocity[Y]                                      0.38617E+00 
c  Velocity[Z]                                      0.30110E+00 
c  Pressure     0.99990E-01    1374   0.42002E-01   0.74769E-01 0.11677E+01 
c  k            0.57470E-01     152   0.33914E-03   0.18412E-03 0.33163E+01 
c  epsilon      0.59627E+03     114   0.12912E-02   0.21189E+06 0.33128E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00078221                             5
a  epsilon                 -4.3288                            18
a  Local Time Step      4.2278e-08                        281739


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.2886          7.3969         0.77277         0.18264
v  Velocity[Y]             -6.5767          13.284         0.58692         0.43427
v  Velocity[Z]              -9.684          6.1666        -0.43679      -0.0043459
v  ǁVelocityǁ            0.0011758          14.436          2.7461          3.5109
v  Pressure                -3911.5           55043           37039           29852
v  k                    2.9075e-08          1.9411        0.016647        0.021605
v  epsilon              0.00064322       1.604e+05          144.06          14.179
v  TurbVisc             8.6994e-14         0.21629      0.00090302        0.013719
v  CourantNb              0.014811      1.3224e+05          165.15          38.184
v  FourierNb                0.2226      2.3653e+06          217.72          2.8658
v  total_pressure       4.9609e+05      5.5504e+05      5.3704e+05      5.2985e+05
v  Local Time Step            0.01        0.056713        0.010001         0.01001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7217      2.3879e+06          382.87           41.05


 TIME FOR THE TIME STEP              317:        0.18730E+03

===============================================================


 INSTANT    0.318000000E+02   TIME STEP NUMBER             318
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall           Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.122623847E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444389E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54725E+01 0.27511E+01
   Friction velocity        uet   :  0.31607E-01 0.41992E+02
   Friction velocity        uk    :  0.31676E-01 0.41992E+02
   Dimensionless distance   yplus :  0.53582E-02 0.12911E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5831
   Nb of faces within the viscous sub-layer     :      20421
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13315E+01     507   0.21581E+00   0.92557E+00 0.26395E+01 
c  Velocity[X]                                      0.23829E+00 
c  Velocity[Y]                                      0.38617E+00 
c  Velocity[Z]                                      0.30110E+00 
c  Pressure     0.99990E-01    1374   0.42002E-01   0.74769E-01 0.11677E+01 
c  k            0.57470E-01     152   0.33914E-03   0.18412E-03 0.33163E+01 
c  epsilon      0.59627E+03     114   0.12912E-02   0.21189E+06 0.33128E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00078221                             5
a  epsilon                 -4.3288                            18
a  Local Time Step      4.2278e-08                        281739


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------v  ǁVelocityǁ            0.0040398          14.597          2.7611          3.5155
v  Pressure                -3867.2           55636           37481           30195
v  k                    2.7799e-08          1.5263        0.016734        0.021642
v  epsilon              0.00066805       1.022e+05          145.31          14.248
v  TurbVisc             1.6915e-13         0.21629      0.00090669        0.013722
v  CourantNb              0.061817      1.3472e+05          166.09          38.274
v  FourierNb               0.22262      2.3653e+06          217.72          2.8662
v  total_pressure       4.9613e+05      5.5564e+05      5.3748e+05       5.302e+05
v  Local Time Step            0.01        0.062384        0.010001         0.01001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6901      2.3841e+06          383.81           41.14


 TIME FOR THE TIME STEP              318:        0.18706E+03

===============================================================


 INSTANT    0.319000000E+02   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        -0.824987714E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444393E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57896E+01 0.27986E+01
   Friction velocity        uet   :  0.26425E-01 0.45056E+02
   Friction velocity        uk    :  0.27268E-01 0.45056E+02
   Dimensionless distance   yplus :  0.49988E-02 0.12804E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5913
   Nb of faces within the viscous sub-layer     :      20290
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13358E+01     500   0.22030E+00   0.82952E+00 0.24925E+01 
c  Velocity[X]                                      0.19713E+00 
c  Velocity[Y]                                      0.35817E+00 
c  Velocity[Z]                                      0.27422E+00 
c  Pressure     0.90806E-01    1337   0.36333E-01   0.66358E-01 0.90109E+00 
c  k            0.57621E-01     151   0.24081E-03   0.14525E-03 0.29407E+01 
c  epsilon      0.60639E+03     108   0.79650E-03   0.66772E+05 0.18499E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.6993e-05                             5
a  epsilon                -0.45049                            10
a  Local Time Step      4.2278e-08                        281739


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.4494          7.5168         0.77587         0.18381
v  Velocity[Y]             -6.6448          13.269         0.58857         0.43546
v  Velocity[Z]             -9.5419          6.1919        -0.44255      -0.0040067
v  ǁVelocityǁ            0.0014481          14.399          2.7745          3.5203
v  Pressure                -3895.8           56139           37855           30484
v  k                    3.7375e-08        v  ǁVelocityǁ            0.0040398          14.597          2.7611          3.5155
v  Pressure                -3867.2           55636           37481           30195
v  k                    2.7799e-08          1.5263        0.016734        0.021642
v  epsilon              0.00066805       1.022e+05          145.31          14.248
v  TurbVisc             1.6915e-13         0.21629      0.00090669        0.013722
v  CourantNb              0.061817      1.3472e+05          166.09          38.274
v  FourierNb               0.22262      2.3653e+06          217.72          2.8662
v  total_pressure       4.9613e+05      5.5564e+05      5.3748e+05       5.302e+05
v  Local Time Step            0.01        0.062384        0.010001         0.01001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6901      2.3841e+06          383.81           41.14


 TIME FOR THE TIME STEP              318:        0.18356E+03

===============================================================


 INSTANT    0.319000000E+02   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        -0.824987714E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444393E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57896E+01 0.27986E+01
   Friction velocity        uet   :  0.26425E-01 0.45056E+02
   Friction velocity        uk    :  0.27268E-01 0.45056E+02
   Dimensionless distance   yplus :  0.49988E-02 0.12804E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5913
   Nb of faces within the viscous sub-layer     :      20290
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
------------------------c  Velocity     0.13355E+01     500   0.21308E+00   0.82461E+00 0.24821E+01 
c  Velocity[X]                                      0.17837E+00 
c  Velocity[Y]                                      0.39589E+00 
c  Velocity[Z]                                      0.25035E+00 
c  Pressure     0.88053E-01    1317   0.34230E-01   0.63704E-01 0.74795E+00 
c  k            0.57667E-01     137   0.22816E-03   0.11135E-03 0.25728E+01 
c  epsilon      0.60332E+03     100   0.77063E-03   0.47682E+05 0.15648E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.5108e-05                             5
a  epsilon                 -5.1388                            17
a  Local Time Step      4.2278e-08                        281743


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5401          7.5726         0.77559         0.18375
v  Velocity[Y]             -6.6152          11.819         0.59457         0.43586
v  Velocity[Z]             -9.6016          6.7906        -0.44685      -0.0039225
v  ǁVelocityǁ            0.0029858          12.779          2.7876          3.5242
v  Pressure                -3933.4           56561           38169           30721
v  k                    3.3104e-08          1.4893         0.01706        0.021714
v  epsilon               0.0012357           99027          150.46          14.462
v  TurbVisc             1.9896e-13         0.21629      0.00091206        0.013728
v  CourantNb              0.021224      1.4773e+05           167.7          38.445
v  FourierNb                0.2227      2.3653e+06          217.73          2.8666
v  total_pressure       4.9607e+05      5.5656e+05      5.3817e+05      5.3072e+05
v  Local Time Step            0.01        0.075485        0.010001        0.010011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6394       2.367e+06          385.43          41.312


 TIME FOR THE TIME STEP              320:        0.18314E+03

===============================================================


 INSTANT    0.321000000E+02   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         0.267615575E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444383E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55572E+01 0.29008E+01
   Friction velocity        uet   :  0.16926E-01 0.46618E+02
   Friction velocity        uk    :  0.18681E-01 0.46618E+02
   Dimensionless distance   yplus :  0.51117E-02 0.12657E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5975
   Nb of faces within the viscous sub-layer     :      20134
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13371E+01     500   0.21710E+00   0.80923E+00 0.24564E+01 
c  Velocity[X]                                      0.18500E+00 
c  Velocity[Y]                                      0.37002E+00 
c  c  Velocity     0.13355E+01     500   0.21308E+00   0.82461E+00 0.24821E+01 
c  Velocity[X]                                      0.17837E+00 
c  Velocity[Y]                                      0.39589E+00 
c  Velocity[Z]                                      0.25035E+00 
c  Pressure     0.88053E-01    1317   0.34230E-01   0.63704E-01 0.74795E+00 
c  k            0.57667E-01     137   0.22816E-03   0.11135E-03 0.25728E+01 
c  epsilon      0.60332E+03     100   0.77063E-03   0.47682E+05 0.15648E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.5108e-05                             5
a  epsilon                 -5.1388                            17
a  Local Time Step      4.2278e-08                        281743


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5401          7.5726         0.77559         0.18375
v  Velocity[Y]             -6.6152          11.819         0.59457         0.43586
v  Velocity[Z]             -9.6016          6.7906        -0.44685      -0.0039225
v  ǁVelocityǁ            0.0029858          12.779          2.7876          3.5242
v  Pressure                -3933.4           56561           38169           30721
v  k                    3.3104e-08          1.4893         0.01706        0.021714
v  epsilon               0.0012357           99027          150.46          14.462
v  TurbVisc             1.9896e-13         0.21629      0.00091206        0.013728
v  CourantNb              0.021224      1.4773e+05           167.7          38.445
v  FourierNb                0.2227      2.3653e+06          217.73          2.8666
v  total_pressure       4.9607e+05      5.5656e+05      5.3817e+05      5.3072e+05
v  Local Time Step            0.01        0.075485        0.010001        0.010011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6394       2.367e+06          385.43          41.312


 TIME FOR THE TIME STEP              320:        0.18516E+03

===============================================================


 INSTANT    0.321000000E+02   TIME STEP NUMBER             321
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46       Free outlet               3          46         0.156444390E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.80243E+01 0.29050E+01
   Friction velocity        uet   :  0.24045E-01 0.46612E+02
   Friction velocity        uk    :  0.24020E-01 0.46612E+02
   Dimensionless distance   yplus :  0.45896E-02 0.12715E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6011
   Nb of faces within the viscous sub-layer     :      20079
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13401E+01     498   0.21789E+00   0.81595E+00 0.24639E+01 
c  Velocity[X]                                      0.18925E+00 
c  Velocity[Y]                                      0.38132E+00 
c  Velocity[Z]                                      0.24538E+00 
c  Pressure     0.80956E-01    1269   0.30213E-01   0.57529E-01 0.52211E+00 
c  k            0.57784E-01     139   0.21453E-03   0.11143E-03 0.25696E+01 
c  epsilon      0.61187E+03      93   0.10969E-02   0.68253E+05 0.18165E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.1658e-05                             7
a  epsilon                 -2.2099                            14
a  Local Time Step      4.2278e-08                        281748


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5389          7.6846         0.78077         0.18395
v  Velocity[Y]             -6.6571          11.047         0.60368         0.43637
v  Velocity[Z]              -9.607          6.3854        -0.45292      -0.0036756
v  ǁVelocityǁ            0.0040533          12.017          2.8086          3.5311
v  Pressure                -4073.9           57249           38657           31077
v  k                    3.8995e-08          1.6763        0.017502        0.021776
v  epsilon              0.00043517      1.4396e+05           159.8          14.664
v  TurbVisc             7.7741e-14         0.21629      0.00091753        0.013733
v  CourantNb              0.023048      1.5435e+05          169.25          38.576
v  FourierNb               0.22284      2.3653e+06          217.75          2.8671
v  total_pressure       4.9593e+05      5.5725e+05      5.3866e+05      5.3108e+05
v  Local Time Step            0.01        0.091337        0.010001        0.010011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6482      2.3671e+06          386.99          41.443


 TIME FOR THE TIME STEP              322:        0.17899E+03

===============================================================


 INSTANT    0.323000000E+02   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        -0.289919825E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444384E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface      Free outlet               3          46         0.156444390E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.80243E+01 0.29050E+01
   Friction velocity        uet   :  0.24045E-01 0.46612E+02
   Friction velocity        uk    :  0.24020E-01 0.46612E+02
   Dimensionless distance   yplus :  0.45896E-02 0.12715E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6011
   Nb of faces within the viscous sub-layer     :      20079
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13401E+01     498   0.21789E+00   0.81595E+00 0.24639E+01 
c  Velocity[X]                                      0.18925E+00 
c  Velocity[Y]                                      0.38132E+00 
c  Velocity[Z]                                      0.24538E+00 
c  Pressure     0.80956E-01    1269   0.30213E-01   0.57529E-01 0.52211E+00 
c  k            0.57784E-01     139   0.21453E-03   0.11143E-03 0.25696E+01 
c  epsilon      0.61187E+03      93   0.10969E-02   0.68253E+05 0.18165E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.1658e-05                             7
a  epsilon                 -2.2099                            14
a  Local Time Step      4.2278e-08                        281748


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5389          7.6846         0.78077         0.18395
v  Velocity[Y]             -6.6571          11.047         0.60368         0.43637
v  Velocity[Z]              -9.607          6.3854        -0.45292      -0.0036756
v  ǁVelocityǁ            0.0040533          12.017          2.8086          3.5311
v  Pressure                -4073.9     v  TurbVisc             2.1853e-13         0.21629      0.00091937        0.013735
v  CourantNb             0.0064386      1.4574e+05          169.46          38.637
v  FourierNb               0.22293      2.3653e+06          217.74          2.8668
v  total_pressure       4.9579e+05       5.575e+05      5.3882e+05      5.3119e+05
v  Local Time Step            0.01         0.10047        0.010001        0.010012


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6401      2.3684e+06           387.2          41.504


 TIME FOR THE TIME STEP              323:        0.17842E+03

===============================================================


 INSTANT    0.324000000E+02   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         0.984608711E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444384E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52508E+01 0.30011E+01
   Friction velocity        uet   :  0.29072E-01 0.44827E+02
   Friction velocity        uk    :  0.28830E-01 0.44827E+02
   Dimensionless distance   yplus :  0.41469E-02 0.12589E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6062
   Nb of faces within the viscous sub-layer     :      19956
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13429E+01     492   0.22024E+00   0.84405E+00 0.25016E+01 
c  Velocity[X]                                      0.20600E+00 
c  Velocity[Y]                                      0.38424E+00 
c  Velocity[Z]                                      0.25381E+00 
c  Pressure     0.75410E-01    1225   0.26979E-01   0.52729E-01 0.32518E+00 
c  k            0.57876E-01     136   0.27310E-03   0.10158E-03 0.24510E+01 
c  epsilon      0.62275E+03      97   0.31324E-02   0.15711E+06 0.26556E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.5981e-05                             2
a  epsilon                 -1.5298                            14
a  Local Time Step      4.2278e-08                        281754


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.6279          7.6949         0.78363         0.18397
v  Velocity[Y]             -6.6733          10.553         0.61153         0.43539
v  Velocity[Z]             -9.6106          6.0548        -0.46024      -0.0040179
v  ǁVelocityǁ            0.0024883          11.491           2.829          3.5369
v  Pressure                -4368.6           57718           38958           31282
v  k                    4.5157e-08          2.0605        0.017875        0.021834
v  epsilon              0.00039108      2.2372e+05          168.45          14.817
v  TurbVisc             1.9998e-13         0.21629      0.00092333        0.013738
v  CourantNb              0.049236      1.3776e+05          169.91          38.689
v  FourierNb               0.22299      2.36v  TurbVisc             2.1853e-13         0.21629      0.00091937        0.013735
v  CourantNb             0.0064386      1.4574e+05          169.46          38.637
v  FourierNb               0.22293      2.3653e+06          217.74          2.8668
v  total_pressure       4.9579e+05       5.575e+05      5.3882e+05      5.3119e+05
v  Local Time Step            0.01         0.10047        0.010001        0.010012


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6401      2.3684e+06           387.2          41.504


 TIME FOR THE TIME STEP              323:        0.18055E+03

===============================================================


 INSTANT    0.324000000E+02   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         0.984608711E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444384E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52508E+01 0.30011E+01
   Friction velocity        uet   :  0.29072E-01 0.44827E+02
   Friction velocity        uk    :  0.28830E-01 0.44827E+02
   Dimensionless distance   yplus :  0.41469E-02 0.12589E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6062
   Nb of faces within the viscous sub-layer     :      19956
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13429E+01     492   0.22024E+00   0.84405E+0c  Pressure     0.73488E-01    1158   0.25570E-01   0.50914E-01 0.25458E+00 
c  k            0.57902E-01     150   0.25740E-03   0.13248E-03 0.27971E+01 
c  epsilon      0.62096E+03     118   0.20154E-02   0.10359E+06 0.21858E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.6109e-05                             4
a  epsilon                 -6.2412                            22
a  Local Time Step      4.2278e-08                        281747


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5734          7.7069         0.78525         0.18389
v  Velocity[Y]             -6.6478          10.527         0.61764         0.43465
v  Velocity[Z]             -9.6248          6.4934        -0.46333      -0.0044085
v  ǁVelocityǁ            0.0029691          11.383          2.8398          3.5395
v  Pressure                -4545.2           57901           39056           31348
v  k                    7.7145e-08          1.5998        0.018005        0.021864
v  epsilon              0.00057417      1.2143e+05          167.15          14.883
v  TurbVisc              2.458e-13         0.21629      0.00092688        0.013741
v  CourantNb              0.017915      1.2894e+05          170.34          38.746
v  FourierNb               0.22308      2.3653e+06          217.75          2.8671
v  total_pressure       4.9545e+05       5.579e+05      5.3906e+05      5.3135e+05
v  Local Time Step            0.01         0.11708        0.010001        0.010013


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6936       2.371e+06          388.09          41.613


 TIME FOR THE TIME STEP              325:        0.17417E+03

===============================================================


 INSTANT    0.326000000E+02   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         0.104740664E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444384E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52157E+01 0.29940E+01
   Friction velocity        uet   :  0.30772E-01 0.41900E+02
   Friction velocity        uk    :  0.33637E-01 0.41900E+02
   Dimensionless distance   yplus :  0.40322E-02 0.12633E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6098
   Nb of faces within the viscous sub-layer     :      19891
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13457E+01     492   0.22672E+00   0.78309E+00 0.24053E+01 
c  Velocity[X]                                      0.21785E+00 
c  Velocity[Y]                                      0.34123E+00 
c  Velocity[Z]                                      0.22401E+00 
c  Pressure     0.72545E-01    1086   0.24773E-01   0.49850E-01 0.19129E+00 
c  k            0.57941E-01     143   0.19973E-03   0.11413E-03 0.25947E+01 
c  epsilon      0.61280E+03      99   0.85257E-03   0.79c  Pressure     0.73488E-01    1158   0.25570E-01   0.50914E-01 0.25458E+00 
c  k            0.57902E-01     150   0.25740E-03   0.13248E-03 0.27971E+01 
c  epsilon      0.62096E+03     118   0.20154E-02   0.10359E+06 0.21858E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.6109e-05                             4
a  epsilon                 -6.2412                            22
a  Local Time Step      4.2278e-08                        281747


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5734          7.7069         0.78525         0.18389
v  Velocity[Y]             -6.6478          10.527         0.61764         0.43465
v  Velocity[Z]             -9.6248          6.4934        -0.46333      -0.0044085
v  ǁVelocityǁ            0.0029691          11.383          2.8398          3.5395
v  Pressure                -4545.2           57901           39056           31348
v  k                    7.7145e-08          1.5998        0.018005        0.021864
v  epsilon              0.00057417      1.2143e+05          167.15          14.883
v  TurbVisc              2.458e-13         0.21629      0.00092688        0.013741
v  CourantNb              0.017915      1.2894e+05          170.34          38.746
v  FourierNb               0.22308      2.3653e+06          217.75          2.8671
v  total_pressure       4.9545e+05       5.579e+05      5.3906e+05      5.3135e+05
v  Local Time Step            0.01         0.11708        0.010001        0.010013


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6936       2.371e+06          388.09          41.613


 TIME FOR THE TIME STEP              325:        0.17484E+03

===============================================================


 INSTANT    0.326000000E+02   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         0.104740664E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46       Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51950E+01 0.29965E+01
   Friction velocity        uet   :  0.30300E-01 0.40662E+02
   Friction velocity        uk    :  0.31989E-01 0.40662E+02
   Dimensionless distance   yplus :  0.44354E-02 0.12539E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6109
   Nb of faces within the viscous sub-layer     :      19857
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13454E+01     494   0.22949E+00   0.81108E+00 0.24464E+01 
c  Velocity[X]                                      0.20665E+00 
c  Velocity[Y]                                      0.37551E+00 
c  Velocity[Z]                                      0.22891E+00 
c  Pressure     0.68889E-01    1029   0.23296E-01   0.46968E-01 0.14381E+00 
c  k            0.57989E-01     147   0.20843E-03   0.12503E-03 0.27137E+01 
c  epsilon      0.61727E+03     100   0.11478E-02   0.12316E+06 0.23297E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.0009e-05                             7
a  epsilon                 -6.9646                            35
a  Local Time Step      4.2278e-08                        281740


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.6121          7.7727         0.78756         0.18329
v  Velocity[Y]             -6.6058          10.133         0.61764         0.43299
v  Velocity[Z]             -9.6627          6.3401        -0.46696      -0.0050208
v  ǁVelocityǁ            0.0055658          11.226          2.8526          3.5443
v  Pressure                -4895.4           58133           39150           31412
v  k                    4.3324e-08          1.8879        0.018288        0.021924
v  epsilon               0.0005402      1.6699e+05          174.14           15.01
v  TurbVisc             8.5983e-14         0.21629      0.00093293        0.013745
v  CourantNb             0.0020159      1.1511e+05          171.52          38.843
v  FourierNb               0.22316      2.3653e+06          217.76           2.868
v  total_pressure        4.951e+05      5.5813e+05      5.3915e+05      5.3141e+05
v  Local Time Step            0.01         0.12174        0.010002        0.010014


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.707      2.3669e+06          389.28          41.711


 TIME FOR THE TIME STEP              327:        0.16036E+03

===============================================================


 INSTANT    0.328000000E+02   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        -0.726671158E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444380E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ----------------------------------Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51950E+01 0.29965E+01
   Friction velocity        uet   :  0.30300E-01 0.40662E+02
   Friction velocity        uk    :  0.31989E-01 0.40662E+02
   Dimensionless distance   yplus :  0.44354E-02 0.12539E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6109
   Nb of faces within the viscous sub-layer     :      19857
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13454E+01     494   0.22949E+00   0.81108E+00 0.24464E+01 
c  Velocity[X]                                      0.20665E+00 
c  Velocity[Y]                                      0.37551E+00 
c  Velocity[Z]                                      0.22891E+00 
c  Pressure     0.68889E-01    1029   0.23296E-01   0.46968E-01 0.14381E+00 
c  k            0.57989E-01     147   0.20843E-03   0.12503E-03 0.27137E+01 
c  epsilon      0.61727E+03     100   0.11478E-02   0.12316E+06 0.23297E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.0009e-05                             7
a  epsilon                 -6.9646                            35
a  Local Time Step      4.2278e-08                        281740


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.6121          7.7727         0.78756         0.18329
v  Velocity[Y]             -6.6058          10.133         0.61764         0.43299
v  Velocity[Z]             -9.6627          6.3401        -0.46696      -0.0050208
v  ǁVelocityǁ            0.0055658          11.226          2.8526          3.5443
v  Pressure                -4895.4           58133           39150           31412
v  k                    4.3324e-08          1.8879        0.018288        0.021924
v  epsilon               0.0005402      1.6699e+05          174.14           15.01
v  TurbVisc             8.5983e-14     v  total_pressure       4.9497e+05       5.582e+05      5.3916e+05      5.3142e+05
v  Local Time Step            0.01         0.12267        0.010002        0.010015


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7019      2.3687e+06          389.44           41.74


 TIME FOR THE TIME STEP              328:        0.15419E+03

===============================================================


 INSTANT    0.329000000E+02   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        -0.598033766E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444388E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52107E+01 0.29870E+01
   Friction velocity        uet   :  0.31551E-01 0.37647E+02
   Friction velocity        uk    :  0.47920E-01 0.37647E+02
   Dimensionless distance   yplus :  0.41345E-02 0.12484E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6139
   Nb of faces within the viscous sub-layer     :      19801
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13484E+01     494   0.22473E+00   0.79372E+00 0.24169E+01 
c  Velocity[X]                                      0.20674E+00 
c  Velocity[Y]                                      0.36292E+00 
c  Velocity[Z]                                      0.22406E+00 
c  Pressure     0.65429E-01     663   0.20994E-01   0.43992E-01 0.90593E-01 
c  k            0.58044E-01     130   0.17979E-03   0.96343E-04 0.23795E+01 
c  epsilon      0.61492E+03      88   0.55478E-03   0.59611E+05 0.16332E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00049652                            10
a  epsilon                 -4.4417                            21
a  Local Time Step      4.2278e-08                        281740


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.8202          7.7511         0.78849         0.18326
v  Velocity[Y]             -6.5922          9.5055           0.615         0.43381
v  Velocity[Z]             -9.5968          6.3909        -0.47043      -0.0049122
v  ǁVelocityǁ             0.010261          11.243          2.8649          3.5488
v  Pressure                -5138.7           58255           39168           31432
v  k                    4.9217e-08          1.7049        0.018391        0.021989
v  epsilon              0.00067945      1.3105e+05          173.43          15.088
v  TurbVisc             2.5396e-13         0.21629      0.00094391        0.013754
v  CourantNb             0.0038648      1.1803e+05          171.69          38.923
v  FourierNb               0.22329      2.3653e+06          217.77           2.869
v  total_pressure       4.9486e+05      5.5826e+05      5.3917e+05      5.3143e+05
v  Local Time Step            0.01         0.12262        0.010002        0.010016


  ** Computed values on cells
     -------v  total_pressure       4.9497e+05       5.582e+05      5.3916e+05      5.3142e+05
v  Local Time Step            0.01         0.12267        0.010002        0.010015


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7019      2.3687e+06          389.44           41.74


 TIME FOR THE TIME STEP              328:        0.15764E+03

===============================================================


 INSTANT    0.329000000E+02   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        -0.598033766E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444388E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52107E+01 0.29870E+01
   Friction velocity        uet   :  0.31551E-01 0.37647E+02
   Friction velocity        uk    :  0.47920E-01 0.37647E+02
   Dimensionless distance   yplus :  0.41345E-02 0.12484E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6139
   Nb of faces within the viscous sub-layer     :      19801
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13484E+01     494   0.22473E+00   0.79372E+00 0.24169E+01 
c  Velocity[X]                                      0.20674E+00 
c  Velocity[Y]                                      0.36292E+00 
c  Velocity[Z]                                      0.22406E+00 
c  Pressure     0.65429E-01     663   0.20994E-01   0.43992E-01 0.90593E-01 
c  k            0.58044E-01 
  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.1743e-05                             7
a  epsilon                 -4.2989                            22
a  Local Time Step      4.2278e-08                        281737


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.8775          7.7904         0.78932         0.18322
v  Velocity[Y]             -6.6091          10.102         0.61543         0.43442
v  Velocity[Z]             -9.7161          6.1473        -0.47261      -0.0048627
v  ǁVelocityǁ            0.0098715          11.403          2.8711          3.5509
v  Pressure                -5229.2           58306           39178           31447
v  k                    4.4851e-08          1.7718         0.01856        0.022024
v  epsilon              0.00064656      1.3882e+05          176.02           15.17
v  TurbVisc              2.166e-13         0.21629       0.0009499        0.013758
v  CourantNb              0.052636      1.2318e+05          172.03          38.957
v  FourierNb               0.22332      2.3653e+06          217.77          2.8699
v  total_pressure       4.9477e+05      5.5831e+05      5.3918e+05      5.3145e+05
v  Local Time Step            0.01         0.12261        0.010002        0.010016


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.642      2.3689e+06           389.8          41.826


 TIME FOR THE TIME STEP              330:        0.15357E+03

===============================================================


 INSTANT    0.331000000E+02   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        -0.137708813E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444388E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52338E+01 0.29829E+01
   Friction velocity        uet   :  0.30371E-01 0.34832E+02
   Friction velocity        uk    :  0.30718E-01 0.34832E+02
   Dimensionless distance   yplus :  0.41826E-02 0.12411E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6144
   Nb of faces within the viscous sub-layer     :      19722
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13515E+01     494   0.23218E+00   0.84329E+00 0.24885E+01 
c  Velocity[X]                                      0.21787E+00 
c  Velocity[Y]                                      0.39388E+00 
c  Velocity[Z]                                      0.23154E+00 
c  Pressure     0.62700E-01    1029   0.18932E-01   0.41646E-01 0.12313E+00 
c  k            0.58168E-01     129   0.47043E-03   0.14014E-03 0.28654E+01 
c  epsilon      0.61858E+03      96   0.69316E-03   0.56847E+05 0.15770E+02 
-----------------------------------------------------------------------------
  
  

  ** 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                   -7.1743e-05                             7
a  epsilon                 -4.2989                            22
a  Local Time Step      4.2278e-08                        281737


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.8775          7.7904         0.78932         0.18322
v  Velocity[Y]             -6.6091          10.102         0.61543         0.43442
v  Velocity[Z]             -9.7161          6.1473        -0.47261      -0.0048627
v  ǁVelocityǁ            0.0098715          11.403          2.8711          3.5509
v  Pressure                -5229.2           58306           39178           31447
v  k                    4.4851e-08          1.7718         0.01856        0.022024
v  epsilon              0.00064656      1.3882e+05          176.02           15.17
v  TurbVisc              2.166e-13         0.21629       0.0009499        0.013758
v  CourantNb              0.052636      1.2318e+05          172.03          38.957
v  FourierNb               0.22332      2.3653e+06          217.77          2.8699
v  total_pressure       4.9477e+05      5.5831e+05      5.3918e+05      5.3145e+05
v  Local Time Step            0.01         0.12261        0.010002        0.010016


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.642      2.3689e+06           389.8          41.826


 TIME FOR THE TIME STEP              330:        0.15876E+03

===============================================================


 INSTANT    0.331000000E+02   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        -0.137708813E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444388E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52556E+01 0.29981E+01
   Friction velocity        uet   :  0.56673E-02 0.33408E+02
   Friction velocity        uk    :  0.84707E-02 0.33408E+02
   Dimensionless distance   yplus :  0.39962E-02 0.12438E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6150
   Nb of faces within the viscous sub-layer     :      19689
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13521E+01     489   0.22636E+00   0.97719E+00 0.26774E+01 
c  Velocity[X]                                      0.21987E+00 
c  Velocity[Y]                                      0.49891E+00 
c  Velocity[Z]                                      0.25841E+00 
c  Pressure     0.62523E-01    1101   0.18224E-01   0.41340E-01 0.15050E+00 
c  k            0.58245E-01     132   0.31031E-03   0.14451E-03 0.29072E+01 
c  epsilon      0.62633E+03      99   0.12599E-02   0.60178E+05 0.16007E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.2502e-05                             7
a  epsilon                 -4.7894                            23
a  Local Time Step      4.2278e-08                        281743


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.9194          7.8163         0.79059         0.18352
v  Velocity[Y]             -6.6259          9.8007         0.61664         0.43472
v  Velocity[Z]             -9.5457          6.5452        -0.47463      -0.0046311
v  ǁVelocityǁ            0.0083099          11.344          2.8822          3.5537
v  Pressure                -5310.9           58464           39265           31529
v  k                    4.0277e-08           1.782        0.018939        0.022101
v  epsilon              0.00033955      1.4012e+05          181.05          15.313
v  TurbVisc             2.4496e-13         0.21629      0.00096875        0.013769
v  CourantNb              0.098455      1.3077e+05          173.08          39.019
v  FourierNb               0.22346      2.3653e+06           217.8          2.8711
v  total_pressure       4.9469e+05      5.5846e+05      5.3927e+05      5.3153e+05
v  Local Time Step            0.01        0.097797        0.010002        0.010016


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6809      2.3705e+06          390.88           41.89


 TIME FOR THE TIME STEP              332:        0.17110E+03

===============================================================


 INSTANT    0.333000000E+02   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        -0.145129040E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444379E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53072E+01 0.30043E+01
   Friction velocity        uet   :  0.29425E-01 0.33726E+02
   Friction velocity       ------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52556E+01 0.29981E+01
   Friction velocity        uet   :  0.56673E-02 0.33408E+02
   Friction velocity        uk    :  0.84707E-02 0.33408E+02
   Dimensionless distance   yplus :  0.39962E-02 0.12438E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6150
   Nb of faces within the viscous sub-layer     :      19689
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13521E+01     489   0.22636E+00   0.97719E+00 0.26774E+01 
c  Velocity[X]                                      0.21987E+00 
c  Velocity[Y]                                      0.49891E+00 
c  Velocity[Z]                                      0.25841E+00 
c  Pressure     0.62523E-01    1101   0.18224E-01   0.41340E-01 0.15050E+00 
c  k            0.58245E-01     132   0.31031E-03   0.14451E-03 0.29072E+01 
c  epsilon      0.62633E+03      99   0.12599E-02   0.60178E+05 0.16007E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.2502e-05                             7
a  epsilon                 -4.7894                            23
a  Local Time Step      4.2278e-08                        281743


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.9194          7.8163         0.79059         0.18352
v  Velocity[Y]             -6.6259          9.8007         0.61664         0.43472
v  Velocity[Z]             -9.5457          6.5452        -0.47463      -0.0046311
v  ǁVelocityǁ            0.0083099          11.344          2.8822          3.5537
v  Pressure                -5310.9           58464           39265           31529
v  k                    4.0277e-08           1.782        0.018939        0.022101
v  epsilon              0.00033955      1.4012e+05          181.05          15.313
v  TurbVisc             2.4496e-13         0.21629      0.00096875        0.013769
v  CourantNb              0.098455      1.3077e+05          173.08          39.019
v  FourierNb               0.22346      2.3653e+06           217.8          2.8711
v  total_pressure       4.9469e+05      5.5846e+05      5.3927e+05      5.3153e+05
v  Local Time Step    ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5755      2.3867e+06          390.92          41.925


 TIME FOR THE TIME STEP              333:        0.16840E+03

===============================================================


 INSTANT    0.334000000E+02   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        -0.599635767E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444391E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53753E+01 0.30028E+01
   Friction velocity        uet   :  0.31835E-01 0.32657E+02
   Friction velocity        uk    :  0.34948E-01 0.32657E+02
   Dimensionless distance   yplus :  0.40183E-02 0.12381E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6187
   Nb of faces within the viscous sub-layer     :      19619
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13537E+01     486   0.22866E+00   0.11006E+01 0.28391E+01 
c  Velocity[X]                                      0.26938E+00 
c  Velocity[Y]                                      0.55747E+00 
c  Velocity[Z]                                      0.27378E+00 
c  Pressure     0.67431E-01    1082   0.18962E-01   0.44167E-01 0.12951E+00 
c  k            0.58287E-01     134   0.19036E-03   0.13245E-03 0.27812E+01 
c  epsilon      0.63070E+03      96   0.49479E-03   0.44257E+05 0.13672E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -6.318e-05                             4
a  epsilon                 -3.2341                            20
a  Local Time Step      4.2278e-08                        281735


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.9636          7.7584         0.79059         0.18413
v  Velocity[Y]             -6.6343          9.7636         0.62662         0.43519
v  Velocity[Z]             -9.6087          6.1463        -0.48022      -0.0048259
v  ǁVelocityǁ             0.006792          11.354          2.8972          3.5562
v  Pressure                -5358.8           58631           39373           31618
v  k                    6.7878e-08          1.7908        0.019298        0.022148
v  epsilon              0.00064215      1.4091e+05          183.38          15.411
v  TurbVisc             3.0055e-13         0.21629      0.00098838        0.013779
v  CourantNb              0.026095      1.3807e+05           173.8          39.078
v  FourierNb                0.2237      2.3653e+06          217.82          2.8723
v  total_pressure       4.9464e+05      5.5863e+05      5.3937e+05      5.3162e+05
v  Local Time Step            0.01         0.11184        0.010002        0.010018


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6233      2.3822e+06          391.62          41.951


 TIME FOR THE TIME STEP              334:    ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5755      2.3867e+06          390.92          41.925


 TIME FOR THE TIME STEP              333:        0.16664E+03

===============================================================


 INSTANT    0.334000000E+02   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        -0.599635767E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444391E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53753E+01 0.30028E+01
   Friction velocity        uet   :  0.31835E-01 0.32657E+02
   Friction velocity        uk    :  0.34948E-01 0.32657E+02
   Dimensionless distance   yplus :  0.40183E-02 0.12381E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6187
   Nb of faces within the viscous sub-layer     :      19619
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13537E+01     486   0.22866E+00   0.11006E+01 0.28391E+01 
c  Velocity[X]                                      0.26938E+00 
c  Velocity[Y]                                      0.55747E+00 
c  Velocity[Z]                                      0.27378E+00 
c  Pressure     0.67431E-01    1082   0.18962E-01   0.44167E-01 0.12951E+00 
c  k            0.58287E-01     134   0.19036E-03   0.13245E-03 0.27812E+01 
c  epsilon      0.63070E+03      96   0.49479E-03   0.44257E+05 0.13672E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     a  epsilon                 -4.3634                            15
a  Local Time Step      4.2278e-08                        281732


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.9145          7.7628         0.78927         0.18449
v  Velocity[Y]             -6.5926          10.513         0.63019         0.43542
v  Velocity[Z]             -9.4687          6.4044        -0.48209      -0.0048138
v  ǁVelocityǁ            0.0088501          11.665          2.9048          3.5571
v  Pressure                -5396.9           58706           39423           31656
v  k                    6.8418e-08          1.7095        0.019429        0.022159
v  epsilon              0.00060529      1.3228e+05          187.12          15.453
v  TurbVisc                3.5e-13         0.21629       0.0010018        0.013781
v  CourantNb              0.020714      1.4212e+05          174.53          39.096
v  FourierNb               0.22374      2.3653e+06          217.83          2.8734
v  total_pressure        4.946e+05      5.5871e+05      5.3942e+05      5.3166e+05
v  Local Time Step            0.01         0.12269        0.010002         0.01002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6717      2.3771e+06          392.36          41.969


 TIME FOR THE TIME STEP              335:        0.16865E+03

===============================================================


 INSTANT    0.336000000E+02   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         0.310401848E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444391E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55429E+01 0.30260E+01
   Friction velocity        uet   :  0.22243E-01 0.32479E+02
   Friction velocity        uk    :  0.29769E-01 0.32479E+02
   Dimensionless distance   yplus :  0.32264E-02 0.12369E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6218
   Nb of faces within the viscous sub-layer     :      19574
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13547E+01     485   0.23174E+00   0.89394E+00 0.25583E+01 
c  Velocity[X]                                      0.21990E+00 
c  Velocity[Y]                                      0.43712E+00 
c  Velocity[Z]                                      0.23692E+00 
c  Pressure     0.63607E-01    1009   0.18421E-01   0.41363E-01 0.84819E-01 
c  k            0.58391E-01     138   0.18266E-03   0.97457E-04 0.23838E+01 
c  epsilon      0.65044E+03      96   0.10291E-02   0.11480E+06 0.21289E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.5616e-05                             4
a  epsilon                 -2.2754                            14
a  Local Time Step      4.2278e-08                        281735


  ** Computed fields on cells
     ------------------------

   field         a  epsilon                 -4.3634                            15
a  Local Time Step      4.2278e-08                        281732


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.9145          7.7628         0.78927         0.18449
v  Velocity[Y]             -6.5926          10.513         0.63019         0.43542
v  Velocity[Z]             -9.4687          6.4044        -0.48209      -0.0048138
v  ǁVelocityǁ            0.0088501          11.665          2.9048          3.5571
v  Pressure                -5396.9           58706           39423           31656
v  k                    6.8418e-08          1.7095        0.019429        0.022159
v  epsilon              0.00060529      1.3228e+05          187.12          15.453
v  TurbVisc                3.5e-13         0.21629       0.0010018        0.013781
v  CourantNb              0.020714      1.4212e+05          174.53          39.096
v  FourierNb               0.22374      2.3653e+06          217.83          2.8734
v  total_pressure        4.946e+05      5.5871e+05      5.3942e+05      5.3166e+05
v  Local Time Step            0.01         0.12269        0.010002         0.01002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6717      2.3771e+06          392.36          41.969


 TIME FOR THE TIME STEP              335:        0.16684E+03

===============================================================


 INSTANT    0.336000000E+02   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         0.310401848E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444391E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn    ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6218
   Nb of faces within the viscous sub-layer     :      19553
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13513E+01     485   0.22897E+00   0.86901E+00 0.25218E+01 
c  Velocity[X]                                      0.24458E+00 
c  Velocity[Y]                                      0.38000E+00 
c  Velocity[Z]                                      0.24443E+00 
c  Pressure     0.60367E-01     861   0.17229E-01   0.39191E-01 0.45550E-01 
c  k            0.58407E-01     138   0.14603E-03   0.90331E-04 0.22944E+01 
c  epsilon      0.65642E+03      97   0.42658E-03   0.66623E+05 0.16156E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00010059                             6
a  epsilon                 -12.058                             9
a  Local Time Step      4.2278e-08                        281738


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.0148          7.7092         0.78844         0.18452
v  Velocity[Y]             -6.5884          10.645         0.62713         0.43514
v  Velocity[Z]             -9.6552          6.3154        -0.48576      -0.0049557
v  ǁVelocityǁ            0.0097055           11.78          2.9101          3.5576
v  Pressure                -5496.2           58772           39463           31688
v  k                    4.9792e-10          1.7786        0.019693        0.022176
v  epsilon              0.00057706      1.3471e+05           191.1          15.525
v  TurbVisc             3.3475e-13         0.21629       0.0010284        0.013784
v  CourantNb              0.072201      1.5252e+05           175.6          39.109
v  FourierNb               0.22358      2.3653e+06          217.86          2.8751
v  total_pressure        4.945e+05      5.5877e+05      5.3946e+05      5.3169e+05
v  Local Time Step            0.01         0.12272        0.010002        0.010021


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.636      2.3823e+06          393.46          41.984


 TIME FOR THE TIME STEP              337:        0.15918E+03

===============================================================


 INSTANT    0.338000000E+02   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        -0.366431105E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444391E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56020E+01 0.30263E+01
   Friction velocity        uet   :  0.31993E-01 0.31094E+02
   Friction velocity        uk    :  0.31348E-01 0.31094E+02
   Dimensionless distance   yplus :  0.30063E-02 0.12403E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6241
   Nb of faces within the viscous sub-layer     :      19517
   Total number of wall faces    ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6218
   Nb of faces within the viscous sub-layer     :      19553
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13513E+01     485   0.22897E+00   0.86901E+00 0.25218E+01 
c  Velocity[X]                                      0.24458E+00 
c  Velocity[Y]                                      0.38000E+00 
c  Velocity[Z]                                      0.24443E+00 
c  Pressure     0.60367E-01     861   0.17229E-01   0.39191E-01 0.45550E-01 
c  k            0.58407E-01     138   0.14603E-03   0.90331E-04 0.22944E+01 
c  epsilon      0.65642E+03      97   0.42658E-03   0.66623E+05 0.16156E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00010059                             6
a  epsilon                 -12.058                             9
a  Local Time Step      4.2278e-08                        281738


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.0148          7.7092         0.78844         0.18452
v  Velocity[Y]             -6.5884          10.645         0.62713         0.43514
v  Velocity[Z]             -9.6552          6.3154        -0.48576      -0.0049557
v  ǁVelocityǁ            0.0097055           11.78          2.9101          3.5576
v  Pressure                -5496.2           58772           39463           31688
v  k                    4.9792e-10          1.7786        0.019693        0.022176
v  epsilon              0.00057706      1.3471e+05           191.1          15.525
v  TurbVisc             3.3475e-13         0.21629       0.0010284        0.013784
v  CourantNb              0.072201      1.5252e+05           175.6          39.109
v  FourierNb               0.22358      2.3653e+06          217.86          2.8751
v  total_pressure        4.945e+05      5.5877e+05      5.3946e+05      5.3169e+05
v  Local Time Step            0.01         0.12272        0.010002        0.010021


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.636      2.3823e+06          393.46 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.604830334E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444383E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56327E+01 0.30165E+01
   Friction velocity        uet   :  0.31650E-01 0.30707E+02
   Friction velocity        uk    :  0.36160E-01 0.30707E+02
   Dimensionless distance   yplus :  0.24742E-02 0.12384E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6251
   Nb of faces within the viscous sub-layer     :      19508
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13530E+01     480   0.22956E+00   0.77286E+00 0.23771E+01 
c  Velocity[X]                                      0.21637E+00 
c  Velocity[Y]                                      0.34647E+00 
c  Velocity[Z]                                      0.21003E+00 
c  Pressure     0.52809E-01     922   0.14770E-01   0.34153E-01 0.56141E-01 
c  k            0.58469E-01     142   0.18333E-03   0.94518E-04 0.23450E+01 
c  epsilon      0.66235E+03      92   0.61250E-03   0.63173E+05 0.15495E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00026051                             7
a  epsilon                  -2.409                            10
a  Local Time Step      4.2278e-08                        281741


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.0352          7.6764         0.79255         0.18468
v  Velocity[Y]             -6.5985          10.552         0.62891         0.43488
v  Velocity[Z]             -9.7392           6.385        -0.48969      -0.0052863
v  ǁVelocityǁ           0.00073285          11.674          2.9219          3.5588
v  Pressure                -5612.6           58769           39448           31679
v  k                     7.964e-08          1.7727        0.019995        0.022197
v  epsilon               0.0006077      1.3413e+05          195.65          15.611
v  TurbVisc             3.6371e-13         0.21629       0.0010456        0.013786
v  CourantNb               0.06788      1.6342e+05          176.36           39.14
v  FourierNb               0.22348      2.3653e+06          217.89          2.8762
v  total_pressure       4.9439e+05      5.5877e+05      5.3945e+05      5.3168e+05
v  Local Time Step            0.01         0.13708        0.010002         0.01002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6456      2.3706e+06          394.24          42.016


 TIME FOR THE TIME STEP              339:        0.16396E+03

===============================================================


 INSTANT    0.340000000E+02   TIME STEP NUMBER             340
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Bou ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.604830334E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444383E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56327E+01 0.30165E+01
   Friction velocity        uet   :  0.31650E-01 0.30707E+02
   Friction velocity        uk    :  0.36160E-01 0.30707E+02
   Dimensionless distance   yplus :  0.24742E-02 0.12384E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6251
   Nb of faces within the viscous sub-layer     :      19508
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13530E+01     480   0.22956E+00   0.77286E+00 0.23771E+01 
c  Velocity[X]                                      0.21637E+00 
c  Velocity[Y]                                      0.34647E+00 
c  Velocity[Z]                                      0.21003E+00 
c  Pressure     0.52809E-01     922   0.14770E-01   0.34153E-01 0.56141E-01 
c  k            0.58469E-01     142   0.18333E-03   0.94518E-04 0.23450E+01 
c  epsilon      0.66235E+03      92   0.61250E-03   0.63173E+05 0.15495E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00026051                             7
a  epsilon                  -2.409                            10
a  Local Time Step      4.2278e-08                        281741


  ** Computed fiev  Velocity[X]             -4.1561          7.6867         0.79424         0.18478
v  Velocity[Y]             -6.5953          10.112         0.62722         0.43528
v  Velocity[Z]             -9.8325          6.2279         -0.4884      -0.0054901
v  ǁVelocityǁ             0.010748          11.559          2.9246            3.56
v  Pressure                -5684.7           58723           39404           31648
v  k                    5.7801e-08          1.9746        0.020162        0.022211
v  epsilon              0.00060354      1.4893e+05          198.66          15.639
v  TurbVisc             3.9666e-13         0.21629       0.0010616        0.013788
v  CourantNb              0.065021       1.662e+05           176.8          39.146
v  FourierNb               0.22342      2.3653e+06           217.9          2.8773
v  total_pressure       4.9432e+05      5.5872e+05       5.394e+05      5.3165e+05
v  Local Time Step            0.01         0.15078        0.010002        0.010022


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5982      2.3756e+06          394.69          42.024


 TIME FOR THE TIME STEP              340:        0.16441E+03

===============================================================


 INSTANT    0.341000000E+02   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        -0.120941005E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444511E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56495E+01 0.30313E+01
   Friction velocity        uet   :  0.29321E-01 0.28365E+02
   Friction velocity        uk    :  0.29193E-01 0.28365E+02
   Dimensionless distance   yplus :  0.35485E-02 0.12375E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6245
   Nb of faces within the viscous sub-layer     :      19456
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13527E+01     491   0.23153E+00   0.70946E+00 0.22760E+01 
c  Velocity[X]                                      0.20547E+00 
c  Velocity[Y]                                      0.30741E+00 
c  Velocity[Z]                                      0.19657E+00 
c  Pressure     0.50677E-01     996   0.13815E-01   0.32669E-01 0.74199E-01 
c  k            0.58508E-01     129   0.18342E-03   0.10767E-03 0.24988E+01 
c  epsilon      0.66687E+03      84   0.82828E-03   0.79731E+05 0.17175E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00099302                            15
a  epsilon                 -37.685                            26
a  Local Time Step      4.2278e-08                        281736


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.0604          7.6604         0.79314         0.18483
v  Velocity[Y]             -6.5833          10.645          0.6262         0.43564
v  Velocity[Z]             -9.6766          v  Velocity[X]             -4.1561          7.6867         0.79424         0.18478
v  Velocity[Y]             -6.5953          10.112         0.62722         0.43528
v  Velocity[Z]             -9.8325          6.2279         -0.4884      -0.0054901
v  ǁVelocityǁ             0.010748          11.559          2.9246            3.56
v  Pressure                -5684.7           58723           39404           31648
v  k                    5.7801e-08          1.9746        0.020162        0.022211
v  epsilon              0.00060354      1.4893e+05          198.66          15.639
v  TurbVisc             3.9666e-13         0.21629       0.0010616        0.013788
v  CourantNb              0.065021       1.662e+05           176.8          39.146
v  FourierNb               0.22342      2.3653e+06           217.9          2.8773
v  total_pressure       4.9432e+05      5.5872e+05       5.394e+05      5.3165e+05
v  Local Time Step            0.01         0.15078        0.010002        0.010022


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5982      2.3756e+06          394.69          42.024


 TIME FOR THE TIME STEP              340:        0.16562E+03

===============================================================


 INSTANT    0.341000000E+02   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        -0.120941005E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444511E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56495E+01 0.30313E+01
   Friction velocity        uet   :  0.29321E-01 0.28365E+02
   Friction velocity        uk    :  0.29193E-01 0.28365E+02
   Dimensionless distance   yplus :  0.35485E-02 0.12375E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6245
   Nb of       --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13546E+01     487   0.23296E+00   0.71942E+00 0.22916E+01 
c  Velocity[X]                                      0.19176E+00 
c  Velocity[Y]                                      0.32155E+00 
c  Velocity[Z]                                      0.20612E+00 
c  Pressure     0.49990E-01    1010   0.13313E-01   0.32183E-01 0.76982E-01 
c  k            0.58526E-01     128   0.16440E-03   0.92177E-04 0.23104E+01 
c  epsilon      0.66889E+03      82   0.61452E-03   0.53164E+05 0.13952E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.6807e-05                             8
a  epsilon                 -2.4211                            29
a  Local Time Step      4.2278e-08                        281745


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.0731          7.7239         0.79453         0.18481
v  Velocity[Y]             -6.5978          10.368         0.62645         0.43603
v  Velocity[Z]             -9.9366          6.2135        -0.49173      -0.0055178
v  ǁVelocityǁ             0.013161          11.674          2.9278          3.5604
v  Pressure                -5791.3           58666           39344           31606
v  k                    8.1179e-08          1.9861        0.020398        0.022263
v  epsilon              0.00033075       1.528e+05          201.25          15.702
v  TurbVisc             4.0466e-13         0.21629       0.0010988        0.013795
v  CourantNb              0.087381      1.6737e+05          176.69          39.168
v  FourierNb               0.22337      2.3653e+06          217.93          2.8788
v  total_pressure       4.9421e+05      5.5867e+05      5.3934e+05      5.3161e+05
v  Local Time Step            0.01         0.17306        0.010002        0.010021


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6223      2.3719e+06          394.62          42.046


 TIME FOR THE TIME STEP              342:        0.16603E+03

===============================================================


 INSTANT    0.343000000E+02   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        -0.118525231E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444506E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56859E+01 0.30163E+01
   Friction velocity        uet   :  0.31949E-01 0.28164E+02
   Friction velocity        uk    :  0.41759E-01 0.28164E+02
   Dimensionless distance   yplus :  0.26228E-02 0.12373E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6258
   Nb of faces within the viscous sub-layer     :      19458
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
---------------------      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13546E+01     487   0.23296E+00   0.71942E+00 0.22916E+01 
c  Velocity[X]                                      0.19176E+00 
c  Velocity[Y]                                      0.32155E+00 
c  Velocity[Z]                                      0.20612E+00 
c  Pressure     0.49990E-01    1010   0.13313E-01   0.32183E-01 0.76982E-01 
c  k            0.58526E-01     128   0.16440E-03   0.92177E-04 0.23104E+01 
c  epsilon      0.66889E+03      82   0.61452E-03   0.53164E+05 0.13952E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.6807e-05                             8
a  epsilon                 -2.4211                            29
a  Local Time Step      4.2278e-08                        281745


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.0731          7.7239         0.79453         0.18481
v  Velocity[Y]             -6.5978          10.368         0.62645         0.43603
v  Velocity[Z]             -9.9366          6.2135        -0.49173      -0.0055178
v  ǁVelocityǁ             0.013161          11.674          2.9278          3.5604
v  Pressure                -5791.3           58666           39344           31606
v  k                    8.1179e-08          1.9861        0.020398        0.022263
v  epsilon              0.00033075       1.528e+05          201.25          15.702
v  TurbVisc             4.0466e-13         0.21629       0.0010988        0.013795
v  CourantNb              0.087381      1.6737e+05          176.69          39.168
v  FourierNb               0.22337      2.3653e+06          217.93          2.8788
v  total_pressure       4.9421e+05      5.5867e+05      5.3934e+05      5.3161e+05
v  Local Time Step            0.01         0.17306        0.010002        0.010021


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6223      2.3719e+06          394.62          42.046


 TIME FOR THE TIME STEP              342:        0.16372E+03

===============================================================


 INSTANT    0.343000000E+02   TIME STEP NUMBER             343
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ----------Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.383305035E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444503E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56985E+01 0.30297E+01
   Friction velocity        uet   :  0.30571E-01 0.28262E+02
   Friction velocity        uk    :  0.31542E-01 0.28262E+02
   Dimensionless distance   yplus :  0.25752E-02 0.12361E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6258
   Nb of faces within the viscous sub-layer     :      19441
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13544E+01     486   0.22512E+00   0.69526E+00 0.22518E+01 
c  Velocity[X]                                      0.20154E+00 
c  Velocity[Y]                                      0.29684E+00 
c  Velocity[Z]                                      0.19689E+00 
c  Pressure     0.47357E-01     944   0.11912E-01   0.30413E-01 0.47469E-01 
c  k            0.58557E-01     133   0.17607E-03   0.84943E-04 0.22136E+01 
c  epsilon      0.66993E+03      87   0.11794E-02   0.43734E+05 0.12619E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00023847                             8
a  epsilon                 -3.7024                            39
a  Local Time Step      4.2278e-08                        281743


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.1231          7.7156         0.79496          0.1848
v  Velocity[Y]              -6.589           10.39         0.62689         0.43665
v  Velocity[Z]             -9.7202          6.1921        -0.49216      -0.0055401
v  ǁVelocityǁ             0.012852           11.53          2.9335          3.5614
v  Pressure                -5832.9           58627           39311           31580
v  k                    9.6723e-10          1.9405        0.020711        0.022325
v  epsilon              0.00063098      1.4451e+05          202.68          15.751
v  TurbVisc             3.5265e-13         0.21629       0.0011441        0.013807
v  CourantNb              0.031633       1.722e+05          176.77          39.181
v  FourierNb               0.22338      2.3653e+06          217.96          2.8823
v  total_pressure       4.9417e+05      5.5863e+05      5.3931e+05      5.3158e+05
v  Local Time Step            0.01         0.12271        0.010002        0.010021


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6722      2.3758e+06          394.74          42.064


 TIME FOR THE TIME STEP              344:        0.16372E+03

===============================================================


 INSTANT    0.345000000E+02   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        -0.116060065E-17
Rough wall                6           0         0.000000000E+00
Symmetry          Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.383305035E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444503E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56985E+01 0.30297E+01
   Friction velocity        uet   :  0.30571E-01 0.28262E+02
   Friction velocity        uk    :  0.31542E-01 0.28262E+02
   Dimensionless distance   yplus :  0.25752E-02 0.12361E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6258
   Nb of faces within the viscous sub-layer     :      19441
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13544E+01     486   0.22512E+00   0.69526E+00 0.22518E+01 
c  Velocity[X]                                      0.20154E+00 
c  Velocity[Y]                                      0.29684E+00 
c  Velocity[Z]                                      0.19689E+00 
c  Pressure     0.47357E-01     944   0.11912E-01   0.30413E-01 0.47469E-01 
c  k            0.58557E-01     133   0.17607E-03   0.84943E-04 0.22136E+01 
c  epsilon      0.66993E+03      87   0.11794E-02   0.43734E+05 0.12619E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00023847                             8
a  epsilon                 -3.7024                            39
a  Local Time Step      4.2278e-08                        281743


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.1231          7.7156         0.79496          0.1848
v  Velocity[Y]              -6.589       v  Pressure                -5834.6           58621           39304           31572
v  k                     7.929e-08          1.9169        0.020915        0.022359
v  epsilon              0.00015817      1.4403e+05          202.47          15.781
v  TurbVisc             1.1122e-16         0.21629       0.0011699        0.013815
v  CourantNb              0.030711      1.7437e+05          177.08          39.196
v  FourierNb               0.22342      2.3653e+06          217.98          2.8839
v  total_pressure       4.9417e+05      5.5862e+05       5.393e+05      5.3157e+05
v  Local Time Step            0.01         0.12271        0.010002         0.01002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6587      2.3779e+06          395.07           42.08


 TIME FOR THE TIME STEP              345:        0.15938E+03

===============================================================


 INSTANT    0.346000000E+02   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        -0.705453753E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444502E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57913E+01 0.30409E+01
   Friction velocity        uet   :  0.31716E-01 0.27199E+02
   Friction velocity        uk    :  0.32063E-01 0.27199E+02
   Dimensionless distance   yplus :  0.21968E-02 0.12410E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6275
   Nb of faces within the viscous sub-layer     :      19432
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13561E+01     489   0.22844E+00   0.71378E+00 0.22811E+01 
c  Velocity[X]                                      0.21215E+00 
c  Velocity[Y]                                      0.30013E+00 
c  Velocity[Z]                                      0.20150E+00 
c  Pressure     0.49988E-01    1009   0.11907E-01   0.32003E-01 0.62826E-01 
c  k            0.58564E-01     144   0.17437E-03   0.10452E-03 0.24505E+01 
c  epsilon      0.66847E+03      88   0.38250E-03   0.25253E+05 0.96236E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00034323                             6
a  epsilon                 -33.515                            31
a  Local Time Step      4.2278e-08                        281746


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.0549          7.6714         0.79692         0.18493
v  Velocity[Y]             -6.6126          10.708         0.62298         0.43696
v  Velocity[Z]             -9.9066          6.3844        -0.49011      -0.0055245
v  ǁVelocityǁ             0.011308          11.911          2.9302          3.5618
v  Pressure                -5844.4           58591           39280           31550
v  k                    8.2539e-08          1.9476        0.021044        0.022391
v  epsilon              2.1688e-05      1.45v  Pressure                -5834.6           58621           39304           31572
v  k                     7.929e-08          1.9169        0.020915        0.022359
v  epsilon              0.00015817      1.4403e+05          202.47          15.781
v  TurbVisc             1.1122e-16         0.21629       0.0011699        0.013815
v  CourantNb              0.030711      1.7437e+05          177.08          39.196
v  FourierNb               0.22342      2.3653e+06          217.98          2.8839
v  total_pressure       4.9417e+05      5.5862e+05       5.393e+05      5.3157e+05
v  Local Time Step            0.01         0.12271        0.010002         0.01002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6587      2.3779e+06          395.07           42.08


 TIME FOR THE TIME STEP              345:        0.15921E+03

===============================================================


 INSTANT    0.346000000E+02   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        -0.705453753E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444502E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57913E+01 0.30409E+01
   Friction velocity        uet   :  0.31716E-01 0.27199E+02
   Friction velocity        uk    :  0.32063E-01 0.27199E+02
   Dimensionless distance   yplus :  0.21968E-02 0.12410E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6275
   Nb of faces within the viscous sub-layer     :      19432
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs normc  Velocity[X]                                      0.19311E+00 
c  Velocity[Y]                                      0.28742E+00 
c  Velocity[Z]                                      0.19404E+00 
c  Pressure     0.45830E-01     849   0.10953E-01   0.29304E-01 0.37115E-01 
c  k            0.58518E-01     145   0.19161E-03   0.11554E-03 0.25743E+01 
c  epsilon      0.66512E+03      93   0.29710E-03   0.22139E+05 0.90585E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001296                             5
a  epsilon                -0.45193                             4
a  Local Time Step      4.2278e-08                        281741


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.1509          7.6558         0.79716         0.18532
v  Velocity[Y]             -6.6053          10.683         0.62335         0.43693
v  Velocity[Z]             -9.6431          6.4756        -0.49142      -0.0055759
v  ǁVelocityǁ            0.0079459          11.856          2.9304          3.5621
v  Pressure                  -5842           58576           39272           31540
v  k                    8.1916e-08          1.8999        0.021209        0.022412
v  epsilon              0.00067177       1.441e+05          200.93          15.795
v  TurbVisc             4.1508e-13         0.21629       0.0012358         0.01383
v  CourantNb               0.01813      1.7236e+05          176.57          39.189
v  FourierNb                0.2235      2.3653e+06          218.05          2.8875
v  total_pressure       4.9416e+05      5.5858e+05      5.3927e+05      5.3154e+05
v  Local Time Step            0.01          0.1227        0.010002        0.010021


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6795      2.3768e+06          394.62          42.077


 TIME FOR THE TIME STEP              347:        0.15432E+03

===============================================================


 INSTANT    0.348000000E+02   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         0.361714073E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444512E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58249E+01 0.30119E+01
   Friction velocity        uet   :  0.30652E-01 0.25353E+02
   Friction velocity        uk    :  0.31373E-01 0.25353E+02
   Dimensionless distance   yplus :  0.23455E-02 0.12445E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6283
   Nb of faces within the viscous sub-layer     :      19421
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13566E+01     472   0.23080E+00   0.67814E+00 0.22230E+01 
c  Velocity[X]                                      0.19506E+00 
c  Velocity[Y]                                      0.29041E+00 
c  Velocity[Z]                                      0.19267E+00 
c  Pressure    c  Velocity[X]                                      0.19311E+00 
c  Velocity[Y]                                      0.28742E+00 
c  Velocity[Z]                                      0.19404E+00 
c  Pressure     0.45830E-01     849   0.10953E-01   0.29304E-01 0.37115E-01 
c  k            0.58518E-01     145   0.19161E-03   0.11554E-03 0.25743E+01 
c  epsilon      0.66512E+03      93   0.29710E-03   0.22139E+05 0.90585E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001296                             5
a  epsilon                -0.45193                             4
a  Local Time Step      4.2278e-08                        281741


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.1509          7.6558         0.79716         0.18532
v  Velocity[Y]             -6.6053          10.683         0.62335         0.43693
v  Velocity[Z]             -9.6431          6.4756        -0.49142      -0.0055759
v  ǁVelocityǁ            0.0079459          11.856          2.9304          3.5621
v  Pressure                  -5842           58576           39272           31540
v  k                    8.1916e-08          1.8999        0.021209        0.022412
v  epsilon              0.00067177       1.441e+05          200.93          15.795
v  TurbVisc             4.1508e-13         0.21629       0.0012358         0.01383
v  CourantNb               0.01813      1.7236e+05          176.57          39.189
v  FourierNb                0.2235      2.3653e+06          218.05          2.8875
v  total_pressure       4.9416e+05      5.5858e+05      5.3927e+05      5.3154e+05
v  Local Time Step            0.01          0.1227        0.010002        0.010021


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6795      2.3768e+06          394.62          42.077


 TIME FOR THE TIME STEP              347:        0.15363E+03

===============================================================


 INSTANT    0.348000000E+02   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       Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58094E+01 0.30114E+01
   Friction velocity        uet   :  0.15471E-01 0.25237E+02
   Friction velocity        uk    :  0.15462E-01 0.25237E+02
   Dimensionless distance   yplus :  0.20978E-02 0.12433E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6291
   Nb of faces within the viscous sub-layer     :      19421
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13528E+01     456   0.23174E+00   0.70023E+00 0.22592E+01 
c  Velocity[X]                                      0.20831E+00 
c  Velocity[Y]                                      0.29055E+00 
c  Velocity[Z]                                      0.20137E+00 
c  Pressure     0.46574E-01     938   0.10750E-01   0.29717E-01 0.49461E-01 
c  k            0.58480E-01     155   0.18917E-03   0.11566E-03 0.25694E+01 
c  epsilon      0.66051E+03      83   0.23377E-03   0.16125E+05 0.77652E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00022573                             7
a  epsilon                 -23.599                             7
a  Local Time Step      4.2278e-08                        281735


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.1466          7.6641         0.80065         0.18575
v  Velocity[Y]             -6.5551          10.345         0.62532         0.43703
v  Velocity[Z]             -9.8413          6.3828        -0.49312      -0.0056345
v  ǁVelocityǁ              0.00818          11.704          2.9345          3.5622
v  Pressure                -5838.8           58518           39229           31505
v  k                    6.8518e-08           1.893         0.02152        0.022452
v  epsilon              0.00067561      1.3972e+05             200          15.821
v  TurbVisc             3.4318e-13         0.21629       0.0012825        0.013841
v  CourantNb              0.065406       1.745e+05          176.41          39.207
v  FourierNb               0.22342      2.3653e+06          218.08          2.8896
v  total_pressure       4.9416e+05      5.5852e+05      5.3923e+05       5.315e+05
v  Local Time Step            0.01         0.14513        0.010002         0.01002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6156      2.3728e+06          394.49          42.096


 TIME FOR THE TIME STEP              349:        0.15687E+03

===============================================================


 INSTANT    0.350000000E+02   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        -0.482376897E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444504E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined         Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58094E+01 0.30114E+01
   Friction velocity        uet   :  0.15471E-01 0.25237E+02
   Friction velocity        uk    :  0.15462E-01 0.25237E+02
   Dimensionless distance   yplus :  0.20978E-02 0.12433E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6291
   Nb of faces within the viscous sub-layer     :      19421
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13528E+01     456   0.23174E+00   0.70023E+00 0.22592E+01 
c  Velocity[X]                                      0.20831E+00 
c  Velocity[Y]                                      0.29055E+00 
c  Velocity[Z]                                      0.20137E+00 
c  Pressure     0.46574E-01     938   0.10750E-01   0.29717E-01 0.49461E-01 
c  k            0.58480E-01     155   0.18917E-03   0.11566E-03 0.25694E+01 
c  epsilon      0.66051E+03      83   0.23377E-03   0.16125E+05 0.77652E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00022573                             7
a  epsilon                 -23.599                             7
a  Local Time Step      4.2278e-08                        281735


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.1466          7.6641         0.80065         0.18575
v  Velocity[Y]             -6.5551          10.345         0.62532         0.43703
v  Velocity[Z]             -9.8413          6.3828        -0.49312      -0.0056345
v  ǁVelocityǁ              0.00818          11.704          2.9345          3.5622
v  Pressure                -5838.8           58518           39229           31505
v  k                    6.8518e-08     v  CourantNb               0.07682      1.8441e+05          176.75          39.203
v  FourierNb               0.22334      2.3653e+06          218.12          2.8927
v  total_pressure       4.9416e+05       5.585e+05      5.3921e+05      5.3149e+05
v  Local Time Step            0.01          0.1526        0.010002        0.010021


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6571      2.3735e+06          394.87          42.096


 TIME FOR THE TIME STEP              350:        0.15760E+03

===============================================================


 INSTANT    0.351000000E+02   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         0.803616556E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444508E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58183E+01 0.30036E+01
   Friction velocity        uet   :  0.30717E-01 0.33142E+02
   Friction velocity        uk    :  0.35026E-01 0.33142E+02
   Dimensionless distance   yplus :  0.26241E-02 0.12469E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6274
   Nb of faces within the viscous sub-layer     :      19425
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13538E+01     484   0.22663E+00   0.68305E+00 0.22314E+01 
c  Velocity[X]                                      0.20391E+00 
c  Velocity[Y]                                      0.26991E+00 
c  Velocity[Z]                                      0.20923E+00 
c  Pressure     0.43840E-01     799   0.99771E-02   0.27975E-01 0.28815E-01 
c  k            0.58463E-01     159   0.17339E-03   0.93693E-04 0.23064E+01 
c  epsilon      0.65925E+03      95   0.28063E-03   0.26084E+05 0.99047E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0002155                             5
a  epsilon                 -33.709                            14
a  Local Time Step      4.2278e-08                        281738


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.1817          7.6928         0.80187         0.18582
v  Velocity[Y]             -6.5456           10.51         0.62183         0.43721
v  Velocity[Z]             -9.7359          6.4874         -0.4903      -0.0057281
v  ǁVelocityǁ            0.0040955          11.735          2.9293          3.5622
v  Pressure                -5842.8           58481           39204           31487
v  k                    8.5408e-08          1.8934        0.021883        0.022496
v  epsilon              0.00066745        1.42e+05          198.94          15.835
v  TurbVisc             2.7524e-14         0.21629       0.0013709         0.01385
v  CourantNb               0.07173      1.8612e+05          176.46            39.2
v  FourierNb               0.22323      2.3653e+06          218.17          2.8949
v  total_pressure       4.9416e+05      5.58v  CourantNb               0.07682      1.8441e+05          176.75          39.203
v  FourierNb               0.22334      2.3653e+06          218.12          2.8927
v  total_pressure       4.9416e+05       5.585e+05      5.3921e+05      5.3149e+05
v  Local Time Step            0.01          0.1526        0.010002        0.010021


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6571      2.3735e+06          394.87          42.096


 TIME FOR THE TIME STEP              350:        0.16009E+03

===============================================================


 INSTANT    0.351000000E+02   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         0.803616556E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444508E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58183E+01 0.30036E+01
   Friction velocity        uet   :  0.30717E-01 0.33142E+02
   Friction velocity        uk    :  0.35026E-01 0.33142E+02
   Dimensionless distance   yplus :  0.26241E-02 0.12469E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6274
   Nb of faces within the viscous sub-layer     :      19425
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13538E+01     484   0.22663E+00   0.68305E+00 0.22314E+01 
c  Velocity[X]                                      0.20391E+00 
c  Velocity[Y]                                      0.26991E+00 
c  Velocic  epsilon      0.65801E+03      91   0.34759E-03   0.27581E+05 0.10199E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00024266                            16
a  epsilon                 -3.3875                            43
a  Local Time Step      4.2278e-08                        281735


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.1648          7.7077         0.80147         0.18567
v  Velocity[Y]             -6.5654          10.642         0.62146         0.43709
v  Velocity[Z]              -9.989          6.2121        -0.49112      -0.0057363
v  ǁVelocityǁ            0.0075304          11.883          2.9302          3.5621
v  Pressure                -5855.9           58459           39186           31477
v  k                    9.2248e-09          1.9276        0.022051        0.022527
v  epsilon               0.0006793      1.4198e+05          199.35          15.843
v  TurbVisc             4.1131e-13         0.21629       0.0014103        0.013858
v  CourantNb              0.039365      1.8526e+05          176.02            39.2
v  FourierNb               0.22313      2.3653e+06          218.21          2.8969
v  total_pressure       4.9414e+05      5.5846e+05      5.3919e+05      5.3148e+05
v  Local Time Step            0.01         0.10244        0.010002        0.010017


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6918      2.3768e+06          394.23          42.097


 TIME FOR THE TIME STEP              352:        0.15197E+03

===============================================================


 INSTANT    0.353000000E+02   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        -0.862046147E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444507E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57958E+01 0.30091E+01
   Friction velocity        uet   :  0.25081E-01 0.33702E+02
   Friction velocity        uk    :  0.24664E-01 0.33702E+02
   Dimensionless distance   yplus :  0.25916E-02 0.12450E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6274
   Nb of faces within the viscous sub-layer     :      19416
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13543E+01     488   0.23007E+00   0.71336E+00 0.22807E+01 
c  Velocity[X]                                      0.22733E+00 
c  Velocity[Y]                                      0.27433E+00 
c  Velocity[Z]                                      0.21170E+00 
c  Pressure     0.42024E-01     976   0.94214E-02   0.26850E-01 0.55375E-01 
c  k            0.58488E-01     158   0.17417E-03   0.91745E-04 0.22735E+01 
c  epsilon      0.65501E+03      91   0.26237E-03   0.23298E+05 0.94284E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     --------c  epsilon      0.65801E+03      91   0.34759E-03   0.27581E+05 0.10199E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00024266                            16
a  epsilon                 -3.3875                            43
a  Local Time Step      4.2278e-08                        281735


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.1648          7.7077         0.80147         0.18567
v  Velocity[Y]             -6.5654          10.642         0.62146         0.43709
v  Velocity[Z]              -9.989          6.2121        -0.49112      -0.0057363
v  ǁVelocityǁ            0.0075304          11.883          2.9302          3.5621
v  Pressure                -5855.9           58459           39186           31477
v  k                    9.2248e-09          1.9276        0.022051        0.022527
v  epsilon               0.0006793      1.4198e+05          199.35          15.843
v  TurbVisc             4.1131e-13         0.21629       0.0014103        0.013858
v  CourantNb              0.039365      1.8526e+05          176.02            39.2
v  FourierNb               0.22313      2.3653e+06          218.21          2.8969
v  total_pressure       4.9414e+05      5.5846e+05      5.3919e+05      5.3148e+05
v  Local Time Step            0.01         0.10244        0.010002        0.010017


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6918      2.3768e+06          394.23          42.097


 TIME FOR THE TIME STEP              352:        0.16056E+03

===============================================================


 INSTANT    0.353000000E+02   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        -0.862046147E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444507E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57729E+01 0.29939E+01
   Friction velocity        uet   :  0.25315E-01 0.31080E+02
   Friction velocity        uk    :  0.25296E-01 0.31080E+02
   Dimensionless distance   yplus :  0.24505E-02 0.12454E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6272
   Nb of faces within the viscous sub-layer     :      19418
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13563E+01     466   0.22664E+00   0.71072E+00 0.22763E+01 
c  Velocity[X]                                      0.20912E+00 
c  Velocity[Y]                                      0.29338E+00 
c  Velocity[Z]                                      0.20822E+00 
c  Pressure     0.42083E-01     862   0.94486E-02   0.26880E-01 0.32376E-01 
c  k            0.58537E-01     167   0.17934E-03   0.90075E-04 0.22472E+01 
c  epsilon      0.65873E+03      90   0.33016E-03   0.10715E+05 0.63618E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00036149                            14
a  epsilon                 -3.5758                            30
a  Local Time Step      4.2278e-08                        281738


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.1177          7.7487         0.80288         0.18566
v  Velocity[Y]             -6.5024          10.891         0.62424         0.43688
v  Velocity[Z]             -9.9026          6.3031        -0.49442      -0.0056735
v  ǁVelocityǁ             0.011386           12.14          2.9347          3.5622
v  Pressure                -5873.3           58409           39151           31457
v  k                    6.5525e-08          1.9209        0.022446         0.02262
v  epsilon              0.00071693      1.4139e+05          198.59          15.899
v  TurbVisc             4.0357e-13         0.21629       0.0014704        0.013875
v  CourantNb             0.0047595      1.8863e+05          176.56          39.203
v  FourierNb               0.22302      2.3653e+06          218.26          2.9016
v  total_pressure       4.9413e+05      5.5841e+05      5.3915e+05      5.3146e+05
v  Local Time Step            0.01        0.096043        0.010002        0.010016


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier            1.63      2.3691e+06          394.82          42.104


 TIME FOR THE TIME STEP              354:        0.15061E+03

===============================================================


 INSTANT    0.355000000E+02   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        -0.154477645E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444503E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           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 : -0.57729E+01 0.29939E+01
   Friction velocity        uet   :  0.25315E-01 0.31080E+02
   Friction velocity        uk    :  0.25296E-01 0.31080E+02
   Dimensionless distance   yplus :  0.24505E-02 0.12454E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6272
   Nb of faces within the viscous sub-layer     :      19418
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13563E+01     466   0.22664E+00   0.71072E+00 0.22763E+01 
c  Velocity[X]                                      0.20912E+00 
c  Velocity[Y]                                      0.29338E+00 
c  Velocity[Z]                                      0.20822E+00 
c  Pressure     0.42083E-01     862   0.94486E-02   0.26880E-01 0.32376E-01 
c  k            0.58537E-01     167   0.17934E-03   0.90075E-04 0.22472E+01 
c  epsilon      0.65873E+03      90   0.33016E-03   0.10715E+05 0.63618E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00036149                            14
a  epsilon                 -3.5758                            30
a  Local Time Step      4.2278e-08                        281738


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.1177          7.7487         0.80288         0.18566
v  Velocity[Y]             -6.5024          10.891         0.62424         0.43688
v  Velocity[Z]             -9.9026          6.3031        -0.49442      -0.0056735
v  ǁVelocityǁ             0.011386           12.14          2.9347          3.5622
v  Pressure                -5873.3           58409           39151           31457
v  k                    6.5525e-08          1.9209        0.022446         0.02262
v  epsilon              0.00071693      1.4139e+05          198.59          15.899
v  TurbVisc             4.0357e-13         0.21629       0.0014704        0.013875
v  CourantNb             0.0047595      1.8863e+05          176.56          39.203
v  FourierNb               0.22302      
  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5995      2.3699e+06           394.6          42.114


 TIME FOR THE TIME STEP              355:        0.15512E+03

===============================================================


 INSTANT    0.356000000E+02   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         0.347100624E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444511E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57915E+01 0.30040E+01
   Friction velocity        uet   :  0.28886E-01 0.27406E+02
   Friction velocity        uk    :  0.30834E-01 0.27406E+02
   Dimensionless distance   yplus :  0.17733E-02 0.12444E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6270
   Nb of faces within the viscous sub-layer     :      19422
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13549E+01     480   0.22616E+00   0.77308E+00 0.23740E+01 
c  Velocity[X]                                      0.21306E+00 
c  Velocity[Y]                                      0.34513E+00 
c  Velocity[Z]                                      0.21489E+00 
c  Pressure     0.42632E-01     979   0.94860E-02   0.27248E-01 0.67362E-01 
c  k            0.58544E-01     183   0.22988E-03   0.13282E-03 0.27142E+01 
c  epsilon      0.65874E+03      97   0.40826E-03   0.23412E+05 0.93834E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00061037                            26
a  epsilon                 -5.3791                            53
a  Local Time Step      4.2278e-08                        281739


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.1695          7.7031         0.80712         0.18562
v  Velocity[Y]             -6.5475           10.85         0.62177         0.43683
v  Velocity[Z]              -9.739           6.129        -0.49032      -0.0057049
v  ǁVelocityǁ            0.0051387          12.075          2.9354           3.562
v  Pressure                -5900.6           58346           39109           31423
v  k                    7.8712e-08          1.9319        0.022942        0.022725
v  epsilon              0.00015137      1.4271e+05          199.11          15.944
v  TurbVisc             3.0692e-13         0.21629       0.0015714          0.0139
v  CourantNb              0.034615      2.0153e+05          176.67          39.207
v  FourierNb               0.22305      2.3653e+06          218.34          2.9076
v  total_pressure        4.941e+05      5.5835e+05      5.3911e+05      5.3142e+05
v  Local Time Step            0.01        0.094095        0.010002        0.010017


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  -------------
  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5995      2.3699e+06           394.6          42.114


 TIME FOR THE TIME STEP              355:        0.16426E+03

===============================================================


 INSTANT    0.356000000E+02   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         0.347100624E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444511E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57915E+01 0.30040E+01
   Friction velocity        uet   :  0.28886E-01 0.27406E+02
   Friction velocity        uk    :  0.30834E-01 0.27406E+02
   Dimensionless distance   yplus :  0.17733E-02 0.12444E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6270
   Nb of faces within the viscous sub-layer     :      19422
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13549E+01     480   0.22616E+00   0.77308E+00 0.23740E+01 
c  Velocity[X]                                      0.21306E+00 
c  Velocity[Y]                                      0.34513E+00 
c  Velocity[Z]                                      0.21489E+00 
c  Pressure     0.42632E-01     979   0.94860E-02   0.27248E-01 0.67362E-01 
c  k            0.58544E-01     183   0.22988E-03   0.13282E-03 0.27142E+01 
c  epsilon      0.65874E+03      97   0.40826E-03   0.23412E+05 0.93834E+01 
--------------------------  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.4504e-07                             1
a  epsilon                 -39.262                            12
a  Local Time Step      4.2278e-08                        281746


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2072          7.6728         0.80702         0.18562
v  Velocity[Y]             -6.4993          10.463         0.62058         0.43677
v  Velocity[Z]              -9.939          6.4805        -0.49187       -0.005781
v  ǁVelocityǁ               0.0065          11.824          2.9325          3.5622
v  Pressure                -5894.9           58329           39100           31416
v  k                    8.0915e-08          1.8853        0.023204        0.022774
v  epsilon              0.00080273      1.4112e+05          198.87          15.959
v  TurbVisc             4.2096e-13         0.21629       0.0016225        0.013913
v  CourantNb             0.0020725      1.9945e+05          177.31          39.203
v  FourierNb               0.22312      2.3653e+06           218.4          2.9104
v  total_pressure       4.9411e+05      5.5833e+05       5.391e+05      5.3142e+05
v  Local Time Step            0.01          0.1035        0.010002        0.010018


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5961      2.3695e+06          395.71          42.113


 TIME FOR THE TIME STEP              357:        0.15539E+03

===============================================================


 INSTANT    0.358000000E+02   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        -0.632637852E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444507E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58557E+01 0.30091E+01
   Friction velocity        uet   :  0.17565E-01 0.25728E+02
   Friction velocity        uk    :  0.17534E-01 0.25728E+02
   Dimensionless distance   yplus :  0.30441E-02 0.12442E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6254
   Nb of faces within the viscous sub-layer     :      19426
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13544E+01     489   0.22630E+00   0.79202E+00 0.24028E+01 
c  Velocity[X]                                      0.23096E+00 
c  Velocity[Y]                                      0.34897E+00 
c  Velocity[Z]                                      0.21208E+00 
c  Pressure     0.42068E-01     941   0.92831E-02   0.26841E-01 0.44886E-01 
c  k            0.58506E-01     181   0.21903E-03   0.14660E-03 0.28360E+01 
c  epsilon      0.65770E+03      85   0.27269E-03   0.21826E+05 0.90991E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00033192                            12
a  epsilon                 -1.3003                            26
a-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.4504e-07                             1
a  epsilon                 -39.262                            12
a  Local Time Step      4.2278e-08                        281746


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2072          7.6728         0.80702         0.18562
v  Velocity[Y]             -6.4993          10.463         0.62058         0.43677
v  Velocity[Z]              -9.939          6.4805        -0.49187       -0.005781
v  ǁVelocityǁ               0.0065          11.824          2.9325          3.5622
v  Pressure                -5894.9           58329           39100           31416
v  k                    8.0915e-08          1.8853        0.023204        0.022774
v  epsilon              0.00080273      1.4112e+05          198.87          15.959
v  TurbVisc             4.2096e-13         0.21629       0.0016225        0.013913
v  CourantNb             0.0020725      1.9945e+05          177.31          39.203
v  FourierNb               0.22312      2.3653e+06           218.4          2.9104
v  total_pressure       4.9411e+05      5.5833e+05       5.391e+05      5.3142e+05
v  Local Time Step            0.01          0.1035        0.010002        0.010018


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5961      2.3695e+06          395.71          42.113


 TIME FOR THE TIME STEP              357:        0.16387E+03

===============================================================


 INSTANT    0.358000000E+02   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        -0.632637852E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444507E+01
Free inlet               13           0         0.000000000E+00
Convective 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   :  0.20256E-01 0.18842E+02
   Friction velocity        uk    :  0.19968E-01 0.18842E+02
   Dimensionless distance   yplus :  0.24043E-02 0.12442E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6271
   Nb of faces within the viscous sub-layer     :      19411
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13530E+01     479   0.22757E+00   0.85939E+00 0.25033E+01 
c  Velocity[X]                                      0.30300E+00 
c  Velocity[Y]                                      0.32911E+00 
c  Velocity[Z]                                      0.22727E+00 
c  Pressure     0.43052E-01     849   0.94853E-02   0.27458E-01 0.26845E-01 
c  k            0.58507E-01     184   0.25641E-03   0.13031E-03 0.26667E+01 
c  epsilon      0.65707E+03      92   0.35226E-03   0.17051E+05 0.80609E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.1071e-06                             2
a  epsilon               -0.032232                             5
a  Local Time Step      4.2278e-08                        281738


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2803          7.6275         0.80506         0.18612
v  Velocity[Y]             -6.5185          10.346         0.62075         0.43715
v  Velocity[Z]             -9.9319          6.8056         -0.4913      -0.0057676
v  ǁVelocityǁ            0.0042086          11.791          2.9327          3.5618
v  Pressure                -5899.8           58292           39071           31395
v  k                    7.1809e-08          1.8889        0.023505        0.022863
v  epsilon               0.0007266       1.405e+05          197.94          15.998
v  TurbVisc             3.9121e-13         0.21629       0.0017116        0.013941
v  CourantNb              0.043853      1.9287e+05          176.07          39.205
v  FourierNb               0.22328      2.3653e+06          218.47          2.9162
v  total_pressure        4.941e+05      5.5829e+05      5.3907e+05      5.3139e+05
v  Local Time Step            0.01          0.1144        0.010002        0.010018


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5716      2.3671e+06          394.54          42.121


 TIME FOR THE TIME STEP              359:        0.15680E+03

===============================================================


 INSTANT    0.360000000E+02   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         0.523247681E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444513E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58288E+01 0.30185E+01
   Friction velocity        uet   :  0.30912E-01 0.42621E+02
   Friction velocity        uk    :  0.34476E-01 0.42621E+02
   Dimensionless distance   yplus :  0.24732E-02 0.12446E+02
   ------------------------   Friction velocity        uet   :  0.20256E-01 0.18842E+02
   Friction velocity        uk    :  0.19968E-01 0.18842E+02
   Dimensionless distance   yplus :  0.24043E-02 0.12442E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6271
   Nb of faces within the viscous sub-layer     :      19411
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13530E+01     479   0.22757E+00   0.85939E+00 0.25033E+01 
c  Velocity[X]                                      0.30300E+00 
c  Velocity[Y]                                      0.32911E+00 
c  Velocity[Z]                                      0.22727E+00 
c  Pressure     0.43052E-01     849   0.94853E-02   0.27458E-01 0.26845E-01 
c  k            0.58507E-01     184   0.25641E-03   0.13031E-03 0.26667E+01 
c  epsilon      0.65707E+03      92   0.35226E-03   0.17051E+05 0.80609E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.1071e-06                             2
a  epsilon               -0.032232                             5
a  Local Time Step      4.2278e-08                        281738


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2803          7.6275         0.80506         0.18612
v  Velocity[Y]             -6.5185          10.346         0.62075         0.43715
v  Velocity[Z]             -9.9319          6.8056         -0.4913      -0.0057676
v  ǁVelocityǁ            0.0042086          11.791          2.9327          3.5618
v  Pressure                -5899.8           58292           39071           31395
v  k                    7.1809e-08          1.8889        0.023505        0.022863
v  epsilon               0.0007266       1.405e+05          197.94          15.998
v  TurbVisc             3.9121e-13         0.21629       0.0017116        0.013941
v  CourantNb              0.043853      1.9287e+05          176.07          39.205
v  FourierNb               0.22328      2.3653e+06          218.47          2.9162
v  total_pressure        4.941e+05      5.5829e+05      5.3907e+05      5.3139e+05
v  Local Time Step            0.01          0.1144        0.010002        0.010018


  ** Computed values on cells
     ------------------------

   criterion               minimum        TIME FOR THE TIME STEP              360:        0.15706E+03

===============================================================


 INSTANT    0.361000000E+02   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         0.582726030E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444505E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58366E+01 0.29987E+01
   Friction velocity        uet   :  0.29260E-01 0.22109E+02
   Friction velocity        uk    :  0.28936E-01 0.22109E+02
   Dimensionless distance   yplus :  0.17581E-02 0.12435E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6252
   Nb of faces within the viscous sub-layer     :      19415
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13520E+01     502   0.22144E+00   0.92908E+00 0.26027E+01 
c  Velocity[X]                                      0.32978E+00 
c  Velocity[Y]                                      0.35589E+00 
c  Velocity[Z]                                      0.24341E+00 
c  Pressure     0.40546E-01     941   0.89323E-02   0.25872E-01 0.45852E-01 
c  k            0.58530E-01     203   0.30077E-03   0.19732E-03 0.32529E+01 
c  epsilon      0.65948E+03     101   0.94854E-03   0.37164E+05 0.11832E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.0033e-05                            10
a  epsilon                 -1.5074                            30
a  Local Time Step      4.2278e-08                        281746


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2388          7.6388         0.80783         0.18616
v  Velocity[Y]             -6.4724          10.512         0.62572           0.437
v  Velocity[Z]             -9.9029          6.3467         -0.4994      -0.0056471
v  ǁVelocityǁ            0.0066409          11.848          2.9342          3.5619
v  Pressure                -5848.6           58252           39041           31373
v  k                    4.4467e-08          1.8969        0.023981        0.022978
v  epsilon               0.0007363      1.4055e+05          199.31          16.048
v  TurbVisc             2.7196e-13         0.21629       0.0018009        0.013966
v  CourantNb              0.043885      2.1076e+05          176.69          39.206
v  FourierNb               0.22319      2.3653e+06          218.51          2.9221
v  total_pressure       4.9415e+05      5.5825e+05      5.3904e+05      5.3137e+05
v  Local Time Step            0.01         0.11987        0.010002        0.010017


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6446      2.3728e+06           395.2          42.128


 TIME FOR THE TIME STEP              361:        0.16380E+03

===============================================================


 INSTANT    0.362000000E+02   TIME STEP NUMBER             362
 ================== TIME FOR THE TIME STEP              360:        0.16532E+03

===============================================================


 INSTANT    0.361000000E+02   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         0.582726030E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444505E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58366E+01 0.29987E+01
   Friction velocity        uet   :  0.29260E-01 0.22109E+02
   Friction velocity        uk    :  0.28936E-01 0.22109E+02
   Dimensionless distance   yplus :  0.17581E-02 0.12435E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6252
   Nb of faces within the viscous sub-layer     :      19415
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13520E+01     502   0.22144E+00   0.92908E+00 0.26027E+01 
c  Velocity[X]                                      0.32978E+00 
c  Velocity[Y]                                      0.35589E+00 
c  Velocity[Z]                                      0.24341E+00 
c  Pressure     0.40546E-01     941   0.89323E-02   0.25872E-01 0.45852E-01 
c  k            0.58530E-01     203   0.30077E-03   0.19732E-03 0.32529E+01 
c  epsilon      0.65948E+03     101   0.94854E-03   0.37164E+05 0.11832E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.0033e-05             
   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2889          7.7114          0.8106         0.18615
v  Velocity[Y]             -6.5003          10.912         0.62231          0.4372
v  Velocity[Z]             -9.9104          6.2477        -0.49068      -0.0055963
v  ǁVelocityǁ            0.0041913          12.182           2.932          3.5617
v  Pressure                -5819.5           58249           39038           31372
v  k                    5.2432e-08          1.9248        0.024183        0.023054
v  epsilon              0.00039201      1.4341e+05          198.47          16.051
v  TurbVisc             2.0454e-13         0.21629       0.0018718        0.013985
v  CourantNb              0.044882       2.137e+05           176.7           39.21
v  FourierNb               0.22311      2.3653e+06          218.56          2.9268
v  total_pressure       4.9418e+05      5.5825e+05      5.3904e+05      5.3137e+05
v  Local Time Step            0.01         0.13186        0.010002        0.010018


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6484      2.3674e+06          395.27          42.137


 TIME FOR THE TIME STEP              362:        0.14723E+03

===============================================================


 INSTANT    0.363000000E+02   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        -0.290640518E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444511E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58044E+01 0.29960E+01
   Friction velocity        uet   :  0.25930E-01 0.43418E+02
   Friction velocity        uk    :  0.25920E-01 0.43418E+02
   Dimensionless distance   yplus :  0.22090E-02 0.12442E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6248
   Nb of faces within the viscous sub-layer     :      19449
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13554E+01     497   0.23329E+00   0.10039E+01 0.27063E+01 
c  Velocity[X]                                      0.34349E+00 
c  Velocity[Y]                                      0.42267E+00 
c  Velocity[Z]                                      0.23775E+00 
c  Pressure     0.40049E-01     780   0.87872E-02   0.25563E-01 0.22149E-01 
c  k            0.58565E-01     210   0.25713E-03   0.15366E-03 0.28403E+01 
c  epsilon      0.66034E+03     101   0.32555E-03   0.15877E+05 0.77232E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00024509                            12
a  epsilon                 -2.5331                            46
a  Local Time Step      4.2278e-08                        281743


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2624         
   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2889          7.7114          0.8106         0.18615
v  Velocity[Y]             -6.5003          10.912         0.62231          0.4372
v  Velocity[Z]             -9.9104          6.2477        -0.49068      -0.0055963
v  ǁVelocityǁ            0.0041913          12.182           2.932          3.5617
v  Pressure                -5819.5           58249           39038           31372
v  k                    5.2432e-08          1.9248        0.024183        0.023054
v  epsilon              0.00039201      1.4341e+05          198.47          16.051
v  TurbVisc             2.0454e-13         0.21629       0.0018718        0.013985
v  CourantNb              0.044882       2.137e+05           176.7           39.21
v  FourierNb               0.22311      2.3653e+06          218.56          2.9268
v  total_pressure       4.9418e+05      5.5825e+05      5.3904e+05      5.3137e+05
v  Local Time Step            0.01         0.13186        0.010002        0.010018


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6484      2.3674e+06          395.27          42.137


 TIME FOR THE TIME STEP              362:        0.15458E+03

===============================================================


 INSTANT    0.363000000E+02   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        -0.290640518E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444511E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58044E+01 0.29960E+01
   Friction velocity        uet   :  0.25930E-01 0.43418E+02
   Friction velocity        uk    :  0.25920E-01 0.43418E+02
   Dimensionless distance   ypl   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13540E+01     520   0.23010E+00   0.11299E+01 0.28709E+01 
c  Velocity[X]                                      0.40507E+00 
c  Velocity[Y]                                      0.44577E+00 
c  Velocity[Z]                                      0.27906E+00 
c  Pressure     0.42089E-01     862   0.96667E-02   0.26876E-01 0.32336E-01 
c  k            0.58608E-01     223   0.31714E-03   0.21903E-03 0.33664E+01 
c  epsilon      0.66455E+03     103   0.40453E-03   0.37045E+05 0.11705E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00033369                            13
a  epsilon                 -1.4064                            27
a  Local Time Step      4.2278e-08                        281745


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2314          7.6675         0.80082         0.18628
v  Velocity[Y]              -6.509          10.868         0.62699         0.43706
v  Velocity[Z]              -10.03          7.2739        -0.49921      -0.0054486
v  ǁVelocityǁ              0.00561          12.067          2.9373          3.5611
v  Pressure                  -5738           58234           39034           31364
v  k                    5.5962e-08          1.9356        0.024925        0.023247
v  epsilon              0.00089789      1.4332e+05          202.53          16.159
v  TurbVisc             3.3433e-13         0.21629       0.0020026        0.014029
v  CourantNb              0.010976      2.0942e+05          177.85          39.195
v  FourierNb                 0.223      2.3653e+06          218.67          2.9362
v  total_pressure       4.9426e+05      5.5823e+05      5.3903e+05      5.3136e+05
v  Local Time Step            0.01         0.15699        0.010002        0.010015


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6926      2.3671e+06          396.52          42.131


 TIME FOR THE TIME STEP              364:        0.16724E+03

===============================================================


 INSTANT    0.365000000E+02   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         0.132402758E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444508E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57899E+01 0.29926E+01
   Friction velocity        uet   :  0.23244E-01 0.36480E+02
   Friction velocity        uk    :  0.23221E-01 0.36480E+02
   Dimensionless distance   yplus :  0.13173E-02 0.12437E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6267
   Nb of faces within the viscous sub-layer     :      19399
   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     0.13540E+01     520   0.23010E+00   0.11299E+01 0.28709E+01 
c  Velocity[X]                                      0.40507E+00 
c  Velocity[Y]                                      0.44577E+00 
c  Velocity[Z]                                      0.27906E+00 
c  Pressure     0.42089E-01     862   0.96667E-02   0.26876E-01 0.32336E-01 
c  k            0.58608E-01     223   0.31714E-03   0.21903E-03 0.33664E+01 
c  epsilon      0.66455E+03     103   0.40453E-03   0.37045E+05 0.11705E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00033369                            13
a  epsilon                 -1.4064                            27
a  Local Time Step      4.2278e-08                        281745


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2314          7.6675         0.80082         0.18628
v  Velocity[Y]              -6.509          10.868         0.62699         0.43706
v  Velocity[Z]              -10.03          7.2739        -0.49921      -0.0054486
v  ǁVelocityǁ              0.00561          12.067          2.9373          3.5611
v  Pressure                  -5738           58234           39034           31364
v  k                    5.5962e-08          1.9356        0.024925        0.023247
v  epsilon              0.00089789      1.4332e+05          202.53          16.159
v  TurbVisc             3.3433e-13         0.21629       0.0020026        0.014029
v  CourantNb              0.010976      2.0942e+05          177.85          39.195
v  FourierNb                 0.223      2.3653e+06          218.67          2.9362
v  total_pressure       4.9426e+05      5.5823e+05      5.3903e+05      5.3136e+05
v  Local Time Step            0.01         0.15699        0.010002        0.010015


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6926      2.3671e+06          396.52          42.131


 TIME FOR THE TIME STEP              364:        0.17364E+03

==============================================================---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.759035356E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444377E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58549E+01 0.29868E+01
   Friction velocity        uet   :  0.30736E-01 0.33523E+02
   Friction velocity        uk    :  0.38333E-01 0.33523E+02
   Dimensionless distance   yplus :  0.22918E-02 0.12448E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6265
   Nb of faces within the viscous sub-layer     :      19447
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13544E+01     516   0.22628E+00   0.12877E+01 0.30655E+01 
c  Velocity[X]                                      0.46379E+00 
c  Velocity[Y]                                      0.51283E+00 
c  Velocity[Z]                                      0.31113E+00 
c  Pressure     0.41867E-01     830   0.93165E-02   0.26752E-01 0.22086E-01 
c  k            0.58633E-01     232   0.39514E-03   0.33188E-03 0.40797E+01 
c  epsilon      0.66191E+03     101   0.56647E-03   0.50713E+05 0.13809E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0018849                            48
a  epsilon                 -17.396                            69
a  Local Time Step      4.2278e-08                        281750


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.3048          7.6868         0.81102         0.18642
v  Velocity[Y]             -6.4848          10.923         0.61877         0.43713
v  Velocity[Z]             -9.9408           6.579        -0.48515      -0.0055781
v  ǁVelocityǁ            0.0051014          12.179          2.9307          3.5605
v  Pressure                -5665.3           58256           39053           31375
v  k                    3.9526e-08          1.9148        0.025279        0.023476
v  epsilon              0.00068716      1.4303e+05          198.97          16.223
v  TurbVisc             2.2003e-13         0.21629       0.0021402        0.014085
v  CourantNb             0.0042966      2.0599e+05          176.98          39.204
v  FourierNb               0.22307      2.3653e+06          218.76          2.9456
v  total_pressure       4.9433e+05      5.5826e+05      5.3905e+05      5.3138e+05
v  Local Time Step            0.01         0.15413        0.010002        0.010014


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7264      2.3773e+06          395.74           42.15


 TIME FOR THE TIME STEP              366:        0.16324E+03

===============================================================


 INSTANT    0.367000000E+02   TIME STEP NUMBER             367
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                 ---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.759035356E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444377E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58549E+01 0.29868E+01
   Friction velocity        uet   :  0.30736E-01 0.33523E+02
   Friction velocity        uk    :  0.38333E-01 0.33523E+02
   Dimensionless distance   yplus :  0.22918E-02 0.12448E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6265
   Nb of faces within the viscous sub-layer     :      19447
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13544E+01     516   0.22628E+00   0.12877E+01 0.30655E+01 
c  Velocity[X]                                      0.46379E+00 
c  Velocity[Y]                                      0.51283E+00 
c  Velocity[Z]                                      0.31113E+00 
c  Pressure     0.41867E-01     830   0.93165E-02   0.26752E-01 0.22086E-01 
c  k            0.58633E-01     232   0.39514E-03   0.33188E-03 0.40797E+01 
c  epsilon      0.66191E+03     101   0.56647E-03   0.50713E+05 0.13809E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0018849                            48
a  epsilon                 -17.396                            69
a  Local Time Step      4.2278e-08                        281750


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  ---v  Velocity[Z]             -9.9086          6.0162         -0.4906      -0.0056093
v  ǁVelocityǁ            0.0077502          11.829          2.9369          3.5609
v  Pressure                -5649.3           58213           39020           31350
v  k                    3.9267e-08           1.904        0.025667        0.023578
v  epsilon              0.00063244       1.398e+05          202.07           16.26
v  TurbVisc             2.3811e-13         0.21629       0.0022137        0.014117
v  CourantNb              0.011654      2.0582e+05          177.61          39.187
v  FourierNb               0.22309      2.3653e+06           218.8          2.9512
v  total_pressure       4.9435e+05      5.5821e+05      5.3902e+05      5.3135e+05
v  Local Time Step            0.01         0.11923        0.010001        0.010013


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6332       2.373e+06          396.41          42.138


 TIME FOR THE TIME STEP              367:        0.16942E+03

===============================================================


 INSTANT    0.368000000E+02   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        -0.369454901E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444510E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58331E+01 0.29982E+01
   Friction velocity        uet   :  0.31168E-01 0.40608E+02
   Friction velocity        uk    :  0.30405E-01 0.40608E+02
   Dimensionless distance   yplus :  0.18307E-02 0.12440E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6274
   Nb of faces within the viscous sub-layer     :      19395
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13537E+01     530   0.22517E+00   0.12481E+01 0.30176E+01 
c  Velocity[X]                                      0.45105E+00 
c  Velocity[Y]                                      0.49367E+00 
c  Velocity[Z]                                      0.30338E+00 
c  Pressure     0.41860E-01     998   0.96820E-02   0.26744E-01 0.57642E-01 
c  k            0.58680E-01     244   0.41014E-03   0.25452E-03 0.35174E+01 
c  epsilon      0.66149E+03     113   0.49024E-03   0.50263E+05 0.13716E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00047702                            17
a  epsilon                 -4.4612                            29
a  Local Time Step      4.2278e-08                        281737


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2561          7.6884         0.80452         0.18692
v  Velocity[Y]             -6.4662          10.845         0.63015         0.43687
v  Velocity[Z]             -9.9366          6.3303        -0.50115      -0.0053414
v  ǁVelocityǁ            0.0029754           12.04          2.9346           3.561
v  Pressure                -5636.8        v  Velocity[Z]             -9.9086          6.0162         -0.4906      -0.0056093
v  ǁVelocityǁ            0.0077502          11.829          2.9369          3.5609
v  Pressure                -5649.3           58213           39020           31350
v  k                    3.9267e-08           1.904        0.025667        0.023578
v  epsilon              0.00063244       1.398e+05          202.07           16.26
v  TurbVisc             2.3811e-13         0.21629       0.0022137        0.014117
v  CourantNb              0.011654      2.0582e+05          177.61          39.187
v  FourierNb               0.22309      2.3653e+06           218.8          2.9512
v  total_pressure       4.9435e+05      5.5821e+05      5.3902e+05      5.3135e+05
v  Local Time Step            0.01         0.11923        0.010001        0.010013


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6332       2.373e+06          396.41          42.138


 TIME FOR THE TIME STEP              367:        0.17258E+03

===============================================================


 INSTANT    0.368000000E+02   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        -0.369454901E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444510E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58331E+01 0.29982E+01
   Friction velocity        uet   :  0.31168E-01 0.40608E+02
   Friction velocity        uk    :  0.30405E-01 0.40608E+02
   Dimensionless distance   yplus :  0.18307E-02 0.12440E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6274
   Nb of faces within the viscous sub-layer     :      19395
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13537E+01     530   0.22517E+00   0.12481E+01 0.30176E+01 
c  Velocity[X]                                      0.45105E+00 
c  Velocity[Y]                                      0.49367E+00 
c  Velocity[Z]                                      0.30338E+00 
c  Pressure     0.41860E-01     998   0.96820E-02   0.26744E-01 0.57642E-01 
c  k            0.58680E-01     244   0.41014E-03   0.25452E-03 0.35174E+01 
c  epsilon      0.66149E+03     113   0.49024E-03   0.50263E+05 0.13716E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00047702                            17
a  epsilon                 -4.4612                            29
a  Local Time Step      4.2278e-08                        281737


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2561          7.6884         0.80452         0.18692
v  Velocity[Y]             -6.4662          10.845         0.63015         0.43687
v  Velocity[Z]             -9.9366          6.3303        -0.50115      -0.0053414
v  ǁVelocityǁ            0.0029754           12.04          2.9346           3.561
v  Pressure                -5636.8           58185           38992           31332
v  k                    2.6036e-08           1.917        0.026045        0.023695
v  epsilon              0.00071152      1.4177e+05          201.38          16.332
v  TurbVisc             2.3717e-13         0.21629       0.0023011        0.014145
v  CourantNb              0.095947      2.2063e+05           177.7          39.198
v  FourierNb               0.22308      2.3653e+06          218.88          2.9569
v  total_pressure       4.9436e+05      5.5818e+05      5.3899e+05      5.3133e+05
v  Local Time Step            0.01        0.087823        0.010001        0.010013


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6817      2.3702e+06          396.58          42.155


 TIME FOR THE TIME STEP              368:        0.17084E+03

===============================================================


 INSTANT    0.369000000E+02   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         0.651888529E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444518E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58294E+01 0.29767E+01
   Friction velocity        uet   :  0.31434E-01 0.46726E+02
   Friction velocity        uk    :  0.33672E-01 0.46726E+02
   Dimensionless distance   yplus :  0.15169E-02 0.12437E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6270
   Nb of faces within the viscous sub-layer     :      19385
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13511E+01     515   0.22403E+00   0.13616E+01 0.31518E+01 
c  Velocity[X]                                      0.51520E+00 
c  Velocity[Y]                                      0.53250E+00 
c  Velocity[Z]                                      0.31394E+00 
c  Pressure     0.41723E-01     688   0.92287E-02   0.26672E-01 0.25506E-01 
c  k            0.58701E-01     238   0.44084E-03   0.29609E-03 0.37654E+01 
c  epsilon      0.65754E+03     115   0.67706E-03   0.56554E+05 0.14619E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0010718                            85
a  epsilon                 -7.4136                           154
a  Local Time Step      4.2278e-08                        281744


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.3875          7.6865         0.81392         0.18663
v  Velocity[Y]             -6.4562          10.501         0.62784         0.43694
v  Velocity[Z]             -9.8628          5.9707        -0.49429      -0.0053033
v  ǁVelocityǁ            0.0037176          11.807           2.932           3.561
v  Pressure                -5614.4           58192           38994           31335
v  k                    4.4306e-08          1.8898        0.026377        0.023803
v  epsilon              1.1192e-05        1.37e+05          201.71          16.383
v  TurbVisc             1.5083e-13         0.21629       0.0023717        0.014173
v  CourantNb              0.019719      2.1592e+05          177.47          39.206
v  FourierNb               0.22303      2.3653e+06          218.92          2.9617
v  total_pressure       4.9439e+05      5.5819e+05      5.3899e+05      5.3134e+05
v  Local Time Step            0.01        0.076641        0.010001        0.010013


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6764      2.3728e+06          396.39          42.167


 TIME FOR THE TIME STEP              369:        0.16245E+03

===============================================================


 INSTANT    0.370000000E+02   TIME STEP NUMBER             370
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
----------------------------------------------Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444377E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58091E+01 0.29824E+01
   Friction velocity        uet   :  0.32019E-01 0.62589E+02
   Friction velocity        uk    :  0.33561E-01 0.62589E+02
   Dimensionless distance   yplus :  0.13958E-02 0.12419E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6260
   Nb of faces within the viscous sub-layer     :      19465
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13514E+01     489   0.22576E+00   0.12979E+01 0.30773E+01 
c  Velocity[X]                                      0.45733E+00 
c  Velocity[Y]                                      0.51922E+00 
c  Velocity[Z]                                      0.32135E+00 
c  Pressure     0.41525E-01    1009   0.92991E-02   0.26575E-01 0.64342E-01 
c  k            0.58785E-01     259   0.41318E-03   0.23432E-03 0.32925E+01 
c  epsilon      0.66178E+03     120   0.57347E-03   0.45901E+05 0.13068E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00040579                             7
a  epsilon                 -8.1521                            19
a  Local Time Step      4.2278e-08                        281739


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2634          7.6693          0.7974         0.18677
v  Velocity[Y]             -6.4858           10.53         0.62326         0.43706
v  Velocity[Z]             -9.7832          6.8455        -0.49273      -0.0054689
v  ǁVelocityǁ            0.0058106          11.695           2.935          3.5605
v  Pressure                -5580.3           58166           38965           31320
v  k                    3.2896e-08          1.8893        0.026757        0.024036
v  epsilon              0.00086609      1.3826e+05          202.54          16.431
v  TurbVisc             2.0027e-13         0.21629       0.0024835        0.014227
v  CourantNb              0.026137       1.829e+05          177.62          39.183
v  FourierNb               0.22297      2.3653e+06          218.97          2.9709
v  total_pressure       4.9442e+05      5.5817e+05      5.3896e+05      5.3132e+05
v  Local Time Step            0.01        0.091999        0.010002        0.010015


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6733      2.3825e+06          396.59          42.154


 TIME FOR THE TIME STEP              371:        0.16810E+03

===============================================================


 INSTANT    0.372000000E+02   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         0.495840859E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444504E+01
Free inlet               13           0         0.000000000E+00
Convective inlet  Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444377E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58091E+01 0.29824E+01
   Friction velocity        uet   :  0.32019E-01 0.62589E+02
   Friction velocity        uk    :  0.33561E-01 0.62589E+02
   Dimensionless distance   yplus :  0.13958E-02 0.12419E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6260
   Nb of faces within the viscous sub-layer     :      19465
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13514E+01     489   0.22576E+00   0.12979E+01 0.30773E+01 
c  Velocity[X]                                      0.45733E+00 
c  Velocity[Y]                                      0.51922E+00 
c  Velocity[Z]                                      0.32135E+00 
c  Pressure     0.41525E-01    1009   0.92991E-02   0.26575E-01 0.64342E-01 
c  k            0.58785E-01     259   0.41318E-03   0.23432E-03 0.32925E+01 
c  epsilon      0.66178E+03     120   0.57347E-03   0.45901E+05 0.13068E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00040579                             7
a  epsilon                 -8.1521                            19
a  Local Time Step      4.2278e-08                        281739


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2634          7.6693          0.7974         0.18677
v  Velocity[Y]             -6.4858           10.53         0.62326         0.43706
v  Velocity[Z]             -9.7832          6.8455        -0.49273      -0.0054689
v  ǁVelocityǁ            0.0058106     v  epsilon              0.00048029      1.3939e+05          202.64          16.558
v  TurbVisc              1.972e-13         0.21629       0.0025592        0.014258
v  CourantNb             0.0069252      2.1127e+05          177.08          39.189
v  FourierNb               0.22299      2.3653e+06          219.03          2.9759
v  total_pressure       4.9443e+05      5.5817e+05      5.3897e+05      5.3132e+05
v  Local Time Step            0.01          0.1012        0.010002        0.010017


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6857      2.3698e+06          396.11          42.165


 TIME FOR THE TIME STEP              372:        0.16248E+03

===============================================================


 INSTANT    0.373000000E+02   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        -0.107444847E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444389E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58325E+01 0.29856E+01
   Friction velocity        uet   :  0.28762E-01 0.50962E+02
   Friction velocity        uk    :  0.28554E-01 0.50962E+02
   Dimensionless distance   yplus :  0.21187E-02 0.12429E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6281
   Nb of faces within the viscous sub-layer     :      19408
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13521E+01     498   0.22946E+00   0.13799E+01 0.31735E+01 
c  Velocity[X]                                      0.50981E+00 
c  Velocity[Y]                                      0.53878E+00 
c  Velocity[Z]                                      0.33134E+00 
c  Pressure     0.42922E-01     853   0.92066E-02   0.27468E-01 0.26811E-01 
c  k            0.58905E-01     245   0.43615E-03   0.28964E-03 0.36029E+01 
c  epsilon      0.65936E+03     117   0.63548E-03   0.56307E+05 0.14570E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0011883                           111
a  epsilon                 -26.504                           175
a  Local Time Step      4.2278e-08                        281748


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.3106          7.7201         0.81498         0.18631
v  Velocity[Y]             -6.4528          10.329          0.6234         0.43699
v  Velocity[Z]             -9.9669           6.911        -0.48959       -0.005444
v  ǁVelocityǁ            0.0046378          11.908          2.9299          3.5601
v  Pressure                -5556.4           58185           38977           31329
v  k                    2.1262e-08           1.876        0.027279        0.024286
v  epsilon               0.0003102      1.3696e+05          201.18          16.575
v  TurbVisc             1.3376e-13         0.21629       0.0026195        0.014288
v  CourantNb              0.002726      1.99v  epsilon              0.00048029      1.3939e+05          202.64          16.558
v  TurbVisc              1.972e-13         0.21629       0.0025592        0.014258
v  CourantNb             0.0069252      2.1127e+05          177.08          39.189
v  FourierNb               0.22299      2.3653e+06          219.03          2.9759
v  total_pressure       4.9443e+05      5.5817e+05      5.3897e+05      5.3132e+05
v  Local Time Step            0.01          0.1012        0.010002        0.010017


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6857      2.3698e+06          396.11          42.165


 TIME FOR THE TIME STEP              372:        0.16680E+03

===============================================================


 INSTANT    0.373000000E+02   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        -0.107444847E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444389E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58325E+01 0.29856E+01
   Friction velocity        uet   :  0.28762E-01 0.50962E+02
   Friction velocity        uk    :  0.28554E-01 0.50962E+02
   Dimensionless distance   yplus :  0.21187E-02 0.12429E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6281
   Nb of faces within the viscous sub-layer     :      19408
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13521E+01     498   0.22946E+00   0.13799E+01 0.31735E+01 
c  Velocity[X]                                      0.50981E+00 
c  Velocity[Y]                                      0.53878E+00 
c  Velocity[Z]                                      0.33134E+00 
c  Pressure     0.42922E-01     853   0.92066E-02   0.27468E-01 0.26811E-01 
c  k            0.58905E-01     245   0.43615E-03   0.28964E-03 0.36029E+01 
c  epsilon      0.65936E+03     117   0.63548E-03   0.56307E+05 0.14570E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0011883                           111
a  epsilon                 -26.504                           175
a  Local Time Step      4.2278e-08                        281748


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.3106          7.7201         0.81498         0.18631
v  Velocity[Y]             -6.4528          10.329          0.6234         0.43699
v  Velocity[Z]             -9.9669           6.911        -0.48959       -0.005444
v  ǁVelocityǁ            0.0046378          11.908          2.9299          3.5601
v  Pressure                -5556.4           58185           38977           31329
v  k                    2.1262e-08           1.876        0.027279        0.024286
v  epsilon               0.0003102      1.3696e+05          201.18          16.575
v  TurbVisc             1.3376e-13         0.21629       0.0026195        0.014288
v  CourantNb              0.002726      1.9974e+05          177.59           39.21
v  FourierNb               0.22303      2.3653e+06          219.08          2.9804
v  total_pressure       4.9444e+05      5.5818e+05      5.3898e+05      5.3133e+05
v  Local Time Step            0.01        0.089224        0.010002        0.010016


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6966      2.3706e+06          396.67          42.191


 TIME FOR THE TIME STEP              373:        0.16802E+03

===============================================================


 INSTANT    0.374000000E+02   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        -0.110713369E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444374E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58522E+01 0.29864E+01
   Friction velocity        uet   :  0.31235E-01 0.23201E+02
   Friction velocity        uk    :  0.35560E-01 0.23201E+02
   Dimensionless distance   yplus :  0.13633E-02 0.12430E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6262
   Nb of faces within the viscous sub-layer     :      19490
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13536E+01     490   0.22304E+00   0.12527E+01 0.30236E+01 
c  Velocity[X]                                      0.41186E+00 
c  Velocity[Y]                                      0.56201E+00 
c  Velocity[Z]                                      0.27886E+00 
c  Pressure     0.40013E-01     757   0.88039E-02   0.25614E-01 0.22506E-01 
c  k            0.58934E-01     222   0.40403E-03   0.28162E-03 0.35252E+01 
c  epsilon      0.66334E+03      98   0.48532E-03   0.40917E+05 0.12314E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00098023                            60
a  epsilon                 -22.075                           104
a  Local Time Step      4.2278e-08                        281752


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2541          7.7225         0.80707         0.18672
v  Velocity[Y]             -6.4767          10.837         0.61914         0.43737
v  Velocity[Z]             -9.9565          5.9248        -0.48329      -0.0056549
v  ǁVelocityǁ            0.0057239          12.036          2.9321          3.5603
v  Pressure                -5553.3           58183           38973           31325
v  k                    2.1231e-08          1.9121        0.027325          0.0244
v  epsilon              0.00028767      1.4082e+05          201.43          16.592
v  TurbVisc             1.1344e-13         0.21629       0.0026638        0.014314
v  CourantNb            0.00024138      1.8394e+05          176.13          39.187
v  FourierNb               0.22311      2.3653e+06          219.09          2.9843
v  total_pressure       4.9445e+05      5.5818e+05      5.3897e+05      5.3133e+05
v  Local Time Step            0.01        0.098147        0.010002        0.010014


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6699      2.3714e+06          395.22          42.171


 TIME FOR THE TIME STEP              374:        0.16114E+03

===============================================================


 INSTANT    0.375000000E+02   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        -0.664981887E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0       Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58459E+01 0.29831E+01
   Friction velocity        uet   :  0.20292E-01 0.25801E+02
   Friction velocity        uk    :  0.20284E-01 0.25801E+02
   Dimensionless distance   yplus :  0.22778E-02 0.12429E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6265
   Nb of faces within the viscous sub-layer     :      19416
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13543E+01     521   0.22914E+00   0.11778E+01 0.29316E+01 
c  Velocity[X]                                      0.43100E+00 
c  Velocity[Y]                                      0.46424E+00 
c  Velocity[Z]                                      0.28255E+00 
c  Pressure     0.39184E-01     815   0.84320E-02   0.25088E-01 0.26062E-01 
c  k            0.59042E-01     275   0.45374E-03   0.32737E-03 0.37433E+01 
c  epsilon      0.66394E+03     120   0.55870E-03   0.50736E+05 0.13722E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00028577                            31
a  epsilon                 -1.4628                            81
a  Local Time Step      4.2278e-08                        281747


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2978          7.7143         0.81009         0.18652
v  Velocity[Y]             -6.4272          10.547         0.62857         0.43709
v  Velocity[Z]             -10.045          6.1478        -0.49613      -0.0052449
v  ǁVelocityǁ            0.0031744          11.916          2.9285          3.5602
v  Pressure                -5528.8           58190           38970           31323
v  k                    2.7738e-08          1.8991        0.028023        0.024621
v  epsilon              6.3077e-05      1.3935e+05          202.66          16.739
v  TurbVisc             1.3108e-13         0.21629       0.0027819        0.014371
v  CourantNb             0.0044963      1.9926e+05          176.65          39.187
v  FourierNb               0.22326      2.3653e+06          219.19          2.9921
v  total_pressure       4.9447e+05      5.5819e+05      5.3897e+05      5.3132e+05
v  Local Time Step            0.01        0.082444        0.010002        0.010013


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6693      2.3691e+06          395.84          42.179


 TIME FOR THE TIME STEP              376:        0.16155E+03

===============================================================


 INSTANT    0.377000000E+02   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        -0.129728672E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444379E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CFree surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58459E+01 0.29831E+01
   Friction velocity        uet   :  0.20292E-01 0.25801E+02
   Friction velocity        uk    :  0.20284E-01 0.25801E+02
   Dimensionless distance   yplus :  0.22778E-02 0.12429E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6265
   Nb of faces within the viscous sub-layer     :      19416
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13543E+01     521   0.22914E+00   0.11778E+01 0.29316E+01 
c  Velocity[X]                                      0.43100E+00 
c  Velocity[Y]                                      0.46424E+00 
c  Velocity[Z]                                      0.28255E+00 
c  Pressure     0.39184E-01     815   0.84320E-02   0.25088E-01 0.26062E-01 
c  k            0.59042E-01     275   0.45374E-03   0.32737E-03 0.37433E+01 
c  epsilon      0.66394E+03     120   0.55870E-03   0.50736E+05 0.13722E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00028577                            31
a  epsilon                 -1.4628                            81
a  Local Time Step      4.2278e-08                        281747


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2978          7.7143         0.81009         0.18652
v  Velocity[Y]             -6.4272          10.547         0.62857         0.43709
v  Velocity[Z]             -10.045          6.1478        -0.49613      -0.0052449
v  ǁVelocityǁ            0.0031744          11.916          2.9285          3.5602
v  Pressure                -5528.8           58190           38970           31323
v  k                    2.7738e-08          1.8991        0.028023        0.024621
v  epsilon              6.3077e-05     v  FourierNb               0.22327      2.3653e+06          219.23          2.9965
v  total_pressure       4.9448e+05      5.5821e+05      5.3898e+05      5.3133e+05
v  Local Time Step            0.01        0.090688        0.010002        0.010014


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6444      2.3708e+06          395.95          42.182


 TIME FOR THE TIME STEP              377:        0.16258E+03

===============================================================


 INSTANT    0.378000000E+02   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        -0.287712300E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444383E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58357E+01 0.29933E+01
   Friction velocity        uet   :  0.30463E-01 0.42222E+02
   Friction velocity        uk    :  0.29860E-01 0.42222E+02
   Dimensionless distance   yplus :  0.24438E-02 0.12440E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6264
   Nb of faces within the viscous sub-layer     :      19464
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13551E+01     491   0.23449E+00   0.10862E+01 0.28160E+01 
c  Velocity[X]                                      0.36926E+00 
c  Velocity[Y]                                      0.43985E+00 
c  Velocity[Z]                                      0.27707E+00 
c  Pressure     0.40311E-01     741   0.85111E-02   0.25830E-01 0.17912E-01 
c  k            0.59156E-01     228   0.41454E-03   0.19446E-03 0.28644E+01 
c  epsilon      0.66561E+03     112   0.52082E-03   0.36602E+05 0.11580E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00055465                            21
a  epsilon                 -1.7459                            27
a  Local Time Step      4.2278e-08                        281753


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2687          7.7014         0.80309         0.18671
v  Velocity[Y]             -6.4685          10.828         0.62479         0.43737
v  Velocity[Z]              -9.933          6.0216        -0.48883      -0.0054197
v  ǁVelocityǁ            0.0057708           12.11          2.9336          3.5594
v  Pressure                -5519.1           58203           38979           31333
v  k                      1.99e-08          1.9104        0.027994        0.024769
v  epsilon              2.5159e-05      1.4078e+05          203.86          16.785
v  TurbVisc             1.0274e-13         0.21629       0.0028078        0.014414
v  CourantNb              0.031907      1.6777e+05          175.88          39.173
v  FourierNb               0.22329      2.3653e+06          219.17          2.9967
v  total_pressure       4.9448e+05       5.582e+05      5.3898e+05      5.3133e+05
v  Local Time Step            0.01        0.v  FourierNb               0.22327      2.3653e+06          219.23          2.9965
v  total_pressure       4.9448e+05      5.5821e+05      5.3898e+05      5.3133e+05
v  Local Time Step            0.01        0.090688        0.010002        0.010014


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6444      2.3708e+06          395.95          42.182


 TIME FOR THE TIME STEP              377:        0.16360E+03

===============================================================


 INSTANT    0.378000000E+02   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        -0.287712300E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444383E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58357E+01 0.29933E+01
   Friction velocity        uet   :  0.30463E-01 0.42222E+02
   Friction velocity        uk    :  0.29860E-01 0.42222E+02
   Dimensionless distance   yplus :  0.24438E-02 0.12440E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6264
   Nb of faces within the viscous sub-layer     :      19464
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13551E+01     491   0.23449E+00   0.10862E+01 0.28160E+01 
c  Velocity[X]                                      0.36926E+00 
c  Velocity[Y]                                      0.43985E+00 
c  Velocity[Z]                                      0.27707E+00 
c  Pressure     0.40311E-01     741   0.85111E-02   0.25830E-01 0.17912E-01 
c  k            0.59156E-01     228   0.41454E-03   0.19446E-03 0.28644E+01 
c  epsilon      0.66561E+03     112   0.52082E-03   0.36602E+05 0.11580E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00055465                            21
a  epsilon                 -1.7459                            27
a  Local Time Step      4.2278e-08                        281753


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2687          7.7014         0.80309         0.18671
v  Velocity[Y]             -6.4685          10.828         0.62479         0.43737
v  Velocity[Z]              -9.933          6.0216        -0.48883      -0.0054197
v  ǁVelocityǁ            0.0057708           12.11          2.9336          3.5594
v  Pressure                -5519.1           58203           38979           31333
v  k                      1.99e-08          1.9104        0.027994        0.024769
v  epsilon              2.5159e-05      1.4078e+05          203.86          16.785
v  TurbVisc             1.0274e-13         0.21629       0.0028078        0.014414
v  CourantNb              0.031907      1.6777e+05          175.88          39.173
v  FourierNb               0.22329      2.3653e+06          219.17          2.9967
v  total_pressure       4.9448e+05       5.582e+05      5.3898e+05      5.3133e+05
v  Local Time Step            0.01        0.095262        0.010001        0.010013


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6826      2.3724e+06          395.05          42.169


 TIME FOR THE TIME STEP              378:        0.15496E+03

===============================================================


 INSTANT    0.379000000E+02   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        -0.184629560E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444511E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58129E+01 0.30001E+01
   Friction velocity        uet   :  0.25598E-01 0.43305E+02
   Friction velocity        uk    :  0.25505E-01 0.43305E+02
   Dimensionless distance   yplus :  0.29255E-02 0.12406E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6263
   Nb of faces within the viscous sub-layer     :      19407
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13516E+01     508   0.22448E+00   0.11081E+01 0.28436E+01 
c  Velocity[X]                                      0.36574E+00 
c  Velocity[Y]                                      0.46978E+00 
c  Velocity[Z]                                      0.27253E+00 
c  Pressure     0.40124E-01     817   0.88184E-02   0.25717E-01 0.23193E-01 
c  k            0.59219E-01     272   0.44811E-03   0.23377E-03 0.31223E+01 
c  epsilon      0.66572E+03     111   0.55921E-03   0.41869E+05 0.12389E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0005904                            19
a  epsilon                 -1.4021                            25
a  Local Time Step      4.2278e-08                        281752


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.3397          7.7223         0.80503         0.18663
v  Velocity[Y]             -6.4696           10.52         0.63097         0.43689
v  Velocity[Z]             -9.9048          6.3975        -0.49827      -0.0054084
v  ǁVelocityǁ            0.0043238          11.821           2.932          3.5601
v  Pressure                -5527.5           58197           38971           31327
v  k                    2.2429e-08          1.8903        0.028264        0.024855
v  epsilon               0.0008449      1.3868e+05          204.91          16.855
v  TurbVisc              1.547e-13         0.21629       0.0028363        0.014429
v  CourantNb             0.0078099      1.8316e+05          177.07          39.172
v  FourierNb               0.22326      2.3653e+06          219.19          2.9989
v  total_pressure       4.9447e+05       5.582e+05      5.3897e+05      5.3133e+05
v  Local Time Step            0.01         0.10479        0.010002        0.010015


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6332      2.3768e+06          396.26          42.171


 TIME FOR THE TIME STEP              379:        0.16147E+03

===============================================================


 INSTANT    0.380000000E+02   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         0.409018266E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444512E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefi------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58136E+01 0.29981E+01
   Friction velocity        uet   :  0.21127E-01 0.25861E+02
   Friction velocity        uk    :  0.20775E-01 0.25861E+02
   Dimensionless distance   yplus :  0.23537E-02 0.12420E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6238
   Nb of faces within the viscous sub-layer     :      19458
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13524E+01     513   0.23128E+00   0.10180E+01 0.27262E+01 
c  Velocity[X]                                      0.34326E+00 
c  Velocity[Y]                                      0.43709E+00 
c  Velocity[Z]                                      0.23765E+00 
c  Pressure     0.41092E-01     811   0.85924E-02   0.26375E-01 0.20702E-01 
c  k            0.59322E-01     285   0.39868E-03   0.19014E-03 0.27972E+01 
c  epsilon      0.66140E+03     118   0.39044E-03   0.28066E+05 0.10228E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00070091                             5
a  epsilon                 -10.399                            17
a  Local Time Step      4.2278e-08                        281752


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2813          7.7237         0.80891         0.18635
v  Velocity[Y]             -6.4433          10.409         0.62244         0.43674
v  Velocity[Z]             -9.8112          6.1724         -0.4872      -0.0055836
v  ǁVelocityǁ            0.0047818          11.739          2.9313          3.5595
v  Pressure                -5551.5           58209           38973           31332
v  k                    1.3928e-08          1.8815        0.028229        0.024988
v  epsilon              5.1551e-05      1.3672e+05          201.73           16.87
v  TurbVisc             7.6791e-14         0.21629       0.0029329        0.014466
v  CourantNb              0.058068      1.6196e+05          175.42          39.165
v  FourierNb               0.22329      2.3653e+06          219.27          3.0049
v  total_pressure       4.9445e+05      5.5821e+05      5.3897e+05      5.3133e+05
v  Local Time Step            0.01         0.10994        0.010002        0.010014


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6554      2.3728e+06          394.69           42.17


 TIME FOR THE TIME STEP              381:        0.16166E+03

===============================================================


 INSTANT    0.382000000E+02   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        -0.593148797E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444381E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58136E+01 0.29981E+01
   Friction velocity        uet   :  0.21127E-01 0.25861E+02
   Friction velocity        uk    :  0.20775E-01 0.25861E+02
   Dimensionless distance   yplus :  0.23537E-02 0.12420E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6238
   Nb of faces within the viscous sub-layer     :      19458
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13524E+01     513   0.23128E+00   0.10180E+01 0.27262E+01 
c  Velocity[X]                                      0.34326E+00 
c  Velocity[Y]                                      0.43709E+00 
c  Velocity[Z]                                      0.23765E+00 
c  Pressure     0.41092E-01     811   0.85924E-02   0.26375E-01 0.20702E-01 
c  k            0.59322E-01     285   0.39868E-03   0.19014E-03 0.27972E+01 
c  epsilon      0.66140E+03     118   0.39044E-03   0.28066E+05 0.10228E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00070091                             5
a  epsilon                 -10.399                            17
a  Local Time Step      4.2278e-08                        281752


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2813          7.7237         0.80891         0.18635
v  Velocity[Y]             -6.4433          10.409         0.62244         0.43674
v  Velocity[Z]             -9.8112          6.1724         -0.4872      -0.0055836
v  ǁVelocityǁ            0.0047818          11.739          2.9313          3.5595
v  Pressure                -5551.5           58209           38973           31332
v  k                    1.3928e-08          1.8815        0.028229        0.024988
v  epsilon              5.1551e-05      1.3672e+05          201.73           16.87
v  TurbVisc             7.6791e-14         0.21629       0.0029329        0.014466
v  CourantNb              0.058068      1.6196e+05          175.42          39.165
v  FourierNb               0.22329      2.3653e+06          219.27          3.0049
v  total_pressure 
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6657      2.3688e+06          395.68           42.18


 TIME FOR THE TIME STEP              382:        0.16110E+03

===============================================================


 INSTANT    0.383000000E+02   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        -0.533619445E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444511E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57813E+01 0.29923E+01
   Friction velocity        uet   :  0.15642E-01 0.20839E+02
   Friction velocity        uk    :  0.15636E-01 0.20839E+02
   Dimensionless distance   yplus :  0.23788E-02 0.12419E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6263
   Nb of faces within the viscous sub-layer     :      19423
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13511E+01     497   0.23182E+00   0.97431E+00 0.26665E+01 
c  Velocity[X]                                      0.34321E+00 
c  Velocity[Y]                                      0.38689E+00 
c  Velocity[Z]                                      0.24421E+00 
c  Pressure     0.40382E-01     385   0.82264E-02   0.25930E-01 0.15987E-01 
c  k            0.59427E-01     273   0.49610E-03   0.20645E-03 0.28861E+01 
c  epsilon      0.66273E+03     115   0.38129E-03   0.24320E+05 0.95126E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0010268                             8
a  epsilon                 -1.6063                            31
a  Local Time Step      4.2278e-08                        281750


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2651          7.7068         0.81059          0.1857
v  Velocity[Y]             -6.4514          10.481         0.62505         0.43652
v  Velocity[Z]              -9.745          5.9855        -0.49427      -0.0055369
v  ǁVelocityǁ            0.0032238          11.657          2.9269          3.5601
v  Pressure                -5582.1           58197           38958           31327
v  k                    2.0363e-08           1.876        0.028437         0.02514
v  epsilon              0.00021973      1.3725e+05          202.63          16.949
v  TurbVisc             1.0108e-13         0.21629       0.0029234         0.01449
v  CourantNb             0.0023572      1.7008e+05          175.97          39.183
v  FourierNb               0.22349      2.3653e+06          219.25          3.0056
v  total_pressure       4.9442e+05       5.582e+05      5.3896e+05      5.3133e+05
v  Local Time Step            0.01         0.13303        0.010002        0.010016


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.543      2.3
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6657      2.3688e+06          395.68           42.18


 TIME FOR THE TIME STEP              382:        0.15837E+03

===============================================================


 INSTANT    0.383000000E+02   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        -0.533619445E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444511E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57813E+01 0.29923E+01
   Friction velocity        uet   :  0.15642E-01 0.20839E+02
   Friction velocity        uk    :  0.15636E-01 0.20839E+02
   Dimensionless distance   yplus :  0.23788E-02 0.12419E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6263
   Nb of faces within the viscous sub-layer     :      19423
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13511E+01     497   0.23182E+00   0.97431E+00 0.26665E+01 
c  Velocity[X]                                      0.34321E+00 
c  Velocity[Y]                                      0.38689E+00 
c  Velocity[Z]                                      0.24421E+00 
c  Pressure     0.40382E-01     385   0.82264E-02   0.25930E-01 0.15987E-01 
c  k            0.59427E-01     273   0.49610E-03   0.20645E-03 0.28861E+01 
c  epsilon      0.66273E+03     115   0.38129E-03   0.24320E+05 0.95126E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0010268                             8
a  epsilon                 -1.6063                            31
a  Local Time Step      4.2278e-08                        281750


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2651          7.7068         0.81059          0.1857
v  Velocity[Y]             -6.4514          10.481         0.62505         0.43652
v  Velocity[Z]              -9.745          5.9855        -0.49427      -0.0055369
v  ǁVelocityǁ            0.0032238          11.657          2.9269          3.5601
v  Pressure                -5582.1           58197           38958           31327
v  k                    2.0363e-08           1.876        0.028437         0.02514
v  epsilon              0.00021973      1.3725e+05          202.63          16.949
v  TurbVisc             1.0108e-13         0.21629       0.0029234         0.01449
v  CourantNb             0.0023572      1.7008e+05          175.97          39.183
v  FourierNb               0.22349      2.3653e+06          219.25          3.0056
v  total_pressure       4.9442e+05       5.582e+05      5.3896e+05      5.3133e+05
v  Local Time Step            0.01         0.13303        0.010002        0.010016


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.543      2.3726e+06          395.22          42.188


 TIME FOR THE TIME STEP              383:        0.14201E+03

===============================================================


 INSTANT    0.384000000E+02   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         0.391253041E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444484E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57800E+01 0.29738E+01
   Friction velocity        uet   :  0.26189E-01 0.33532E+02
   Friction velocity        uk    :  0.26171E-01 0.33532E+02
   Dimensionless distance   yplus :  0.20620E-02 0.12434E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6271
   Nb of faces within the viscous sub-layer     :      19438
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13535E+01     507   0.22914E+00   0.92574E+00 0.25997E+01 
c  Velocity[X]                                      0.31673E+00 
c  Velocity[Y]                                      0.37650E+00 
c  Velocity[Z]                                      0.23251E+00 
c  Pressure     0.38702E-01     866   0.82029E-02   0.24841E-01 0.28130E-01 
c  k            0.59475E-01     199   0.39357E-03   0.16161E-03 0.25460E+01 
c  epsilon      0.66288E+03     113   0.32215E-03   0.21609E+05 0.89491E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00032231                             7
a  epsilon                 -2.6886                            22
a  Local Time Step      4.2278e-08                        281744


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2024          7.7039         0.81013          0.1857
v  Velocity[Y]              -6.452          10.913         0.62356          0.4368
v  Velocity[Z]             -9.9446          6.9921        -0.48886      -0.0056136
v  ǁVelocityǁ            0.0030076          12.144           2.928          3.5594
v  Pressure                -5595.2           58211           38967           31336
v  k                    1.5816e-08          1.8943        0.028541        0.025201
v  epsilon              0.00095698      1.3887e+05          203.28          16.987
v  TurbVisc             9.1092e-14         0.21629       0.0029648        0.014512
v  CourantNb              0.020021      1.6112e+05          175.77          39.188
v  FourierNb               0.22363      2.3653e+06          219.25           3.009
v  total_pressure        4.944e+05      5.5821e+05      5.3897e+05      5.3134e+05
v  Local Time Step            0.01         0.14633        0.010002        0.010016


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6705      2.3675e+06          395.03          42.197


 TIME FOR THE TIME STEP              384:        0.16035E+03

===============================================================


 INSTANT    0.385000000E+02   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        -0.112589862E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444387E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
----------------------------------   Dimensionless distance   yplus :  0.20088E-02 0.12416E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6262
   Nb of faces within the viscous sub-layer     :      19393
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13548E+01     506   0.22735E+00   0.96736E+00 0.26571E+01 
c  Velocity[X]                                      0.31470E+00 
c  Velocity[Y]                                      0.40924E+00 
c  Velocity[Z]                                      0.24342E+00 
c  Pressure     0.39810E-01     896   0.81971E-02   0.25568E-01 0.26979E-01 
c  k            0.59559E-01     260   0.39451E-03   0.16696E-03 0.25776E+01 
c  epsilon      0.66459E+03     126   0.30683E-03   0.17987E+05 0.81352E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0003453                             8
a  epsilon                 -2.4201                            19
a  Local Time Step      4.2278e-08                        281750


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2608          7.6972         0.80695         0.18594
v  Velocity[Y]             -6.4333          10.876         0.62842          0.4367
v  Velocity[Z]             -9.8782          6.6414        -0.49604      -0.0057463
v  ǁVelocityǁ            0.0069845          12.082           2.928          3.5601
v  Pressure                -5610.9           58200           38954           31325
v  k                    2.1923e-08          1.9019        0.028597        0.025278
v  epsilon              0.00084135      1.3957e+05          204.52          17.073
v  TurbVisc             1.1757e-13         0.21629       0.0029647        0.014528
v  CourantNb              0.031496      1.4926e+05          175.75          39.184
v  FourierNb               0.22385      2.3653e+06          219.25          3.0096
v  total_pressure       4.9439e+05       5.582e+05      5.3895e+05      5.3133e+05
v  Local Time Step            0.01         0.15697        0.010002        0.010018


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6646      2.3701e+06             395          42.193


 TIME FOR THE TIME STEP              386:        0.16080E+03

===============================================================


 INSTANT    0.387000000E+02   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         0.344507172E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444500E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57784E+01 0.29922E+01
   Friction velocity        uet   :  0.26811E-01 0.38077E+02
   Friction velocity        uk    :  0.26440E-01 0.38077E+02
   Dimensionless distance   yplus :  0.32412E-02 0.12425E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6258
   Nb of faces within the visc   Dimensionless distance   yplus :  0.20088E-02 0.12416E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6262
   Nb of faces within the viscous sub-layer     :      19393
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13548E+01     506   0.22735E+00   0.96736E+00 0.26571E+01 
c  Velocity[X]                                      0.31470E+00 
c  Velocity[Y]                                      0.40924E+00 
c  Velocity[Z]                                      0.24342E+00 
c  Pressure     0.39810E-01     896   0.81971E-02   0.25568E-01 0.26979E-01 
c  k            0.59559E-01     260   0.39451E-03   0.16696E-03 0.25776E+01 
c  epsilon      0.66459E+03     126   0.30683E-03   0.17987E+05 0.81352E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0003453                             8
a  epsilon                 -2.4201                            19
a  Local Time Step      4.2278e-08                        281750


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2608          7.6972         0.80695         0.18594
v  Velocity[Y]             -6.4333          10.876         0.62842          0.4367
v  Velocity[Z]             -9.8782          6.6414        -0.49604      -0.0057463
v  ǁVelocityǁ            0.0069845          12.082           2.928          3.5601
v  Pressure                -5610.9           58200           38954           31325
v  k                    2.1923e-08          1.9019        0.028597        0.025278
v  epsilon              0.00084135      1.3957e+05          204.52          17.073
v  TurbVisc             1.1757e-13         0.21629       0.0029647        0.014528
v  CourantNb              0.031496      1.4926e+05          175.75          39.184
v  FourierNb               0.22385      2.3653e+06          219.25          3.0096
v  total_pressure       4.9439e+05       5.582e+05      5.3895e+05      5.3133e+05
v  Local Time Step            0.01         0.15697        0.010002        0.010018


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
    INSTANT    0.388000000E+02   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        -0.298329427E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444391E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57745E+01 0.29896E+01
   Friction velocity        uet   :  0.24326E-01 0.33241E+02
   Friction velocity        uk    :  0.24885E-01 0.33241E+02
   Dimensionless distance   yplus :  0.26884E-02 0.12417E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6263
   Nb of faces within the viscous sub-layer     :      19430
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13547E+01     490   0.22615E+00   0.91825E+00 0.25894E+01 
c  Velocity[X]                                      0.29806E+00 
c  Velocity[Y]                                      0.39476E+00 
c  Velocity[Z]                                      0.22543E+00 
c  Pressure     0.38378E-01     901   0.78706E-02   0.24643E-01 0.30400E-01 
c  k            0.59603E-01     285   0.33361E-03   0.14151E-03 0.23654E+01 
c  epsilon      0.66421E+03     129   0.29151E-03   0.11709E+05 0.65554E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021559                             7
a  epsilon                -0.75798                            11
a  Local Time Step      4.2278e-08                        281750


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.1941          7.6996         0.81007         0.18597
v  Velocity[Y]             -6.4454           10.56         0.62524         0.43674
v  Velocity[Z]             -9.9675          6.5711        -0.49016      -0.0057256
v  ǁVelocityǁ            0.0041618          11.802          2.9337          3.5593
v  Pressure                -5617.6           58220           38967           31336
v  k                    1.3836e-08          1.9135         0.02865        0.025332
v  epsilon               2.153e-05      1.4109e+05           204.2          17.053
v  TurbVisc             5.0842e-14         0.21754       0.0029926        0.014547
v  CourantNb             0.0046247      1.3551e+05          175.46          39.177
v  FourierNb                0.2239      2.3653e+06          219.26          3.0118
v  total_pressure       4.9438e+05      5.5822e+05      5.3897e+05      5.3134e+05
v  Local Time Step            0.01         0.15698        0.010002        0.010018


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6693      2.3762e+06          394.72          42.189


 TIME FOR THE TIME STEP              388:        0.16209E+03

===============================================================


 INSTANT    0.389000000E+02   TIME STEP NUMBER             389
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---- INSTANT    0.388000000E+02   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        -0.298329427E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444391E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57745E+01 0.29896E+01
   Friction velocity        uet   :  0.24326E-01 0.33241E+02
   Friction velocity        uk    :  0.24885E-01 0.33241E+02
   Dimensionless distance   yplus :  0.26884E-02 0.12417E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6263
   Nb of faces within the viscous sub-layer     :      19430
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13547E+01     490   0.22615E+00   0.91825E+00 0.25894E+01 
c  Velocity[X]                                      0.29806E+00 
c  Velocity[Y]                                      0.39476E+00 
c  Velocity[Z]                                      0.22543E+00 
c  Pressure     0.38378E-01     901   0.78706E-02   0.24643E-01 0.30400E-01 
c  k            0.59603E-01     285   0.33361E-03   0.14151E-03 0.23654E+01 
c  epsilon      0.66421E+03     129   0.29151E-03   0.11709E+05 0.65554E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021559                             7
a  epsilon                -0.75798                            11
a  Local Time Step      4.2278e-08                        281750


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.1941          7.6996         0.81007         0.18597
v  Velocity[Y]             -6.4454           10.56         0.62524         0.43674
v  Velocity[Z]             -9.9675          6.5711        -0.49016      -0.0057256
v  ǁVelocityǁ            0.0041618          11.802          2.9337          3.5593
v  Pressure                -5617.6           58220           38967           31336
v  k                    1.3836e-08          1.9135         0.02865        0.025332
v  epsilon               2.153e-05      1.4109e+05           204.2          17.053
v  TurbVisc             5.0842e-14         0.21754       0.0029926        0.014547
v  CourantNb             0.0046247      1.3551e+05          175.46          39.177
v  FourierNb                0.2239      2.3653e+06          219.26          3.0118
v  total_pressure       4.9438e+05      5.5822e+05      5.3897e+05      5.3134e+05
v  Local Time Step            0.01         0.15698        0.010002        0.010018


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6693      2.3762e+06          394.72          42.189


 TIME FOR THE TIME STEP              388:        0.16698E+03

===============================================================


 INSTANT    0.389000000E+02   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         0.255142000E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444384E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57718E+01 0.29980E+01
   Friction velocity        uet   :  0.18155E-01 0.24179E+02
   Friction velocity        uk    :  0.19213E-01 0.24179E+02
   Dimensionless distance   yplus :  0.30852E-02 0.12421E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6253
   Nb of faces within the viscous sub-layer     :      19397
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13526E+01     522   0.22878E+00   0.90143E+00 0.25650E+01 
c  Velocity[X]                                      0.31738E+00 
c  Velocity[Y]                                      0.35416E+00 
c  Velocity[Z]                                      0.22989E+00 
c  Pressure     0.38884E-01     854   0.78549E-02   0.24982E-01 0.24457E-01 
c  k            0.59642E-01     224   0.47562E-03   0.23976E-03 0.30850E+01 
c  epsilon      0.66412E+03     108   0.31205E-03   0.20984E+05 0.87940E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00029434                             8
a  epsilon                 -0.9414                            20
a  Local Time Step      4.2278e-08                        281741


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2447          7.7191         0.81122         0.18589
v  Velocity[Y]             -6.4017          10.689         0.62694         0.43653
v  Velocity[Z]             -9.7317          6.1459        -0.49301      -0.0056722
v  ǁVelocityǁ            0.0051761          11.789          2.9298            3.56
v  Pressure                -5626.9           58209           38956           31328
v  k                    2.0146e-08           1.888        0.028728        0.025329
v  epsilon              0.00082447      1.3847e+05          204.01          17.093
v  TurbVisc              8.581e-14         0.22393        0.003026        0.014555
v  CourantNb              0.043444      1.4239e+05          176.08           39.18
v  FourierNb               0.22391      2.3653e+06          219.31          3.0132
v  total_pressure       4.9437e+05      5.5821e+05      5.3896e+05      5.3133e+05
v  Local Time Step            0.01         0.15696        0.010002        0.010018


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6538      2.3842e+06          395.38          42.193


 TIME FOR THE TIME STEP              389:        0.16206E+03

===============================================================


 INSTANT    0.390000000E+02   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        -0.104712143E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444520E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57607E+01 0.29729E+01
   Friction velocity        uet   :  0.32062E-01 0.38521E+02
   Friction velocity        uk    :  0.34687E-01 0.38521E+02
   Dimensionless distance   yplus :  0.20762E-02 0.12428E+02
   ----------------------------------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13503E+01     517   0.22351E+00   0.89062E+00 0.25498E+01 
c  Velocity[X]                                      0.29897E+00 
c  Velocity[Y]                                      0.35898E+00 
c  Velocity[Z]                                      0.23266E+00 
c  Pressure     0.39331E-01     648   0.79649E-02   0.25253E-01 0.11068E-01 
c  k            0.59624E-01     243   0.42758E-03   0.16213E-03 0.25418E+01 
c  epsilon      0.66184E+03     122   0.33178E-03   0.17733E+05 0.81027E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012514                             5
a  epsilon                 -3.3444                            11
a  Local Time Step      4.2278e-08                        281745


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2001           7.701         0.81208         0.18582
v  Velocity[Y]             -6.4545          10.242         0.62253         0.43656
v  Velocity[Z]             -9.8388          7.1469        -0.48779      -0.0056979
v  ǁVelocityǁ            0.0072949          11.741          2.9317          3.5599
v  Pressure                -5651.8           58227           38964           31335
v  k                    1.7812e-08          1.8735        0.028597        0.025324
v  epsilon              0.00023258      1.3669e+05          203.53           17.07
v  TurbVisc             7.5869e-14         0.22031       0.0030074         0.01455
v  CourantNb               0.04743      1.3372e+05          175.82          39.182
v  FourierNb               0.22399      2.3653e+06          219.28          3.0123
v  total_pressure       4.9435e+05      5.5823e+05      5.3896e+05      5.3133e+05
v  Local Time Step            0.01         0.13544        0.010002        0.010018


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6811      2.3821e+06           395.1          42.194


 TIME FOR THE TIME STEP              391:        0.15638E+03

===============================================================


 INSTANT    0.392000000E+02   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         0.117234941E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444388E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57663E+01 0.29861E+01
   Friction velocity        uet   :  0.24176E-01 0.41492E+02
   Friction velocity        uk    :  0.23845E-01 0.41492E+02
   Dimensionless distance   yplus :  0.23656E-02 0.12415E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6259
   Nb of faces within the viscous sub-layer     :      19403
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
  ------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13503E+01     517   0.22351E+00   0.89062E+00 0.25498E+01 
c  Velocity[X]                                      0.29897E+00 
c  Velocity[Y]                                      0.35898E+00 
c  Velocity[Z]                                      0.23266E+00 
c  Pressure     0.39331E-01     648   0.79649E-02   0.25253E-01 0.11068E-01 
c  k            0.59624E-01     243   0.42758E-03   0.16213E-03 0.25418E+01 
c  epsilon      0.66184E+03     122   0.33178E-03   0.17733E+05 0.81027E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012514                             5
a  epsilon                 -3.3444                            11
a  Local Time Step      4.2278e-08                        281745


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2001           7.701         0.81208         0.18582
v  Velocity[Y]             -6.4545          10.242         0.62253         0.43656
v  Velocity[Z]             -9.8388          7.1469        -0.48779      -0.0056979
v  ǁVelocityǁ            0.0072949          11.741          2.9317          3.5599
v  Pressure                -5651.8           58227           38964           31335
v  k                    1.7812e-08          1.8735        0.028597        0.025324
v  epsilon              0.00023258      1.3669e+05          203.53           17.07
v  TurbVisc             7.5869e-14         0.22031       0.0030074         0.01455
v  CourantNb               0.04743      1.3372e+05          175.82          39.182
v  FourierNb               0.22399      2.3653e+06          219.28          3.0123
v  total_pressure       4.9435e+05      5.5823e+05      5.3896e+05      5.3133e+05
v  Local Time Step            0.01         0.13544        0.010002        0.010018


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6811      2.3821e+06           395.1          42.194


 TIME FOR THE TIME STEP              391:        0.15477E+03

===============================================================


 INSTANT    0.392000000E+02   TIME STEP NUMBER             3Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.120981454E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444513E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57309E+01 0.29960E+01
   Friction velocity        uet   :  0.20060E-01 0.31683E+02
   Friction velocity        uk    :  0.19918E-01 0.31683E+02
   Dimensionless distance   yplus :  0.30642E-02 0.12413E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6253
   Nb of faces within the viscous sub-layer     :      19380
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13520E+01     496   0.22241E+00   0.85448E+00 0.24973E+01 
c  Velocity[X]                                      0.29107E+00 
c  Velocity[Y]                                      0.35251E+00 
c  Velocity[Z]                                      0.21089E+00 
c  Pressure     0.36243E-01     793   0.74395E-02   0.23260E-01 0.15721E-01 
c  k            0.59608E-01     216   0.33328E-03   0.13134E-03 0.22837E+01 
c  epsilon      0.66229E+03     107   0.27511E-03   0.14500E+05 0.73464E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00027164                            28
a  epsilon                 -5.3914                            71
a  Local Time Step      4.2278e-08                        281743


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2486          7.7001         0.81316         0.18582
v  Velocity[Y]             -6.4323          10.668         0.62486         0.43664
v  Velocity[Z]             -9.8081          6.6057        -0.49375      -0.0057151
v  ǁVelocityǁ            0.0055154          11.863           2.929            3.56
v  Pressure                -5662.5           58214           38957           31329
v  k                    1.4551e-08          1.8922        0.028641        0.025328
v  epsilon              0.00044282      1.3772e+05          202.39           17.06
v  TurbVisc             1.1114e-13         0.22425       0.0030301        0.014549
v  CourantNb             0.0086221      1.3251e+05          175.69          39.178
v  FourierNb               0.22416      2.3653e+06          219.32          3.0133
v  total_pressure       4.9434e+05      5.5821e+05      5.3896e+05      5.3133e+05
v  Local Time Step            0.01         0.15697        0.010002        0.010019


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6463      2.3788e+06          395.01          42.192


 TIME FOR THE TIME STEP              393:        0.15915E+03

===============================================================


 INSTANT    0.394000000E+02   TIME STEP NUMBER             394
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall           Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.120981454E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444513E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57309E+01 0.29960E+01
   Friction velocity        uet   :  0.20060E-01 0.31683E+02
   Friction velocity        uk    :  0.19918E-01 0.31683E+02
   Dimensionless distance   yplus :  0.30642E-02 0.12413E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6253
   Nb of faces within the viscous sub-layer     :      19380
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13520E+01     496   0.22241E+00   0.85448E+00 0.24973E+01 
c  Velocity[X]                                      0.29107E+00 
c  Velocity[Y]                                      0.35251E+00 
c  Velocity[Z]                                      0.21089E+00 
c  Pressure     0.36243E-01     793   0.74395E-02   0.23260E-01 0.15721E-01 
c  k            0.59608E-01     216   0.33328E-03   0.13134E-03 0.22837E+01 
c  epsilon      0.66229E+03     107   0.27511E-03   0.14500E+05 0.73464E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00027164                            28
a  epsilon                 -5.3914                            71
a  Local Time Step      4.2278e-08                        281743


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  ---v  Velocity[Z]             -10.001          6.1271        -0.48873      -0.0057094
v  ǁVelocityǁ            0.0045238          12.105          2.9308          3.5593
v  Pressure                -5660.7           58228           38971           31338
v  k                    9.2124e-09          1.8992        0.028649        0.025332
v  epsilon              1.8454e-06      1.3972e+05          203.36          17.057
v  TurbVisc             6.0725e-14         0.22693       0.0030465        0.014552
v  CourantNb             0.0064277      1.2011e+05          175.65          39.186
v  FourierNb               0.22421      2.3653e+06          219.33           3.015
v  total_pressure       4.9434e+05      5.5823e+05      5.3897e+05      5.3134e+05
v  Local Time Step            0.01         0.15698        0.010002        0.010021


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.634      2.3743e+06          394.98          42.201


 TIME FOR THE TIME STEP              394:        0.16512E+03

===============================================================


 INSTANT    0.395000000E+02   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        -0.177674597E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444383E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57382E+01 0.29972E+01
   Friction velocity        uet   :  0.32981E-01 0.37594E+02
   Friction velocity        uk    :  0.32459E-01 0.37594E+02
   Dimensionless distance   yplus :  0.24969E-02 0.12410E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6232
   Nb of faces within the viscous sub-layer     :      19397
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13521E+01     464   0.23039E+00   0.82546E+00 0.24545E+01 
c  Velocity[X]                                      0.26999E+00 
c  Velocity[Y]                                      0.34544E+00 
c  Velocity[Z]                                      0.21003E+00 
c  Pressure     0.37780E-01     672   0.76101E-02   0.24251E-01 0.11083E-01 
c  k            0.59590E-01     272   0.29328E-03   0.11480E-03 0.21281E+01 
c  epsilon      0.66171E+03     123   0.30997E-03   0.15184E+05 0.75027E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.4726e-05                             3
a  epsilon                -0.45408                            13
a  Local Time Step      4.2278e-08                        281748


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2333          7.6974         0.81356         0.18599
v  Velocity[Y]             -6.4838          10.611         0.62383         0.43669
v  Velocity[Z]             -9.7367            6.27        -0.49186      -0.0057847
v  ǁVelocityǁ            0.0050099          11.774          2.9334            3.56
v  Pressure                -5660.1        v  Velocity[Z]             -10.001          6.1271        -0.48873      -0.0057094
v  ǁVelocityǁ            0.0045238          12.105          2.9308          3.5593
v  Pressure                -5660.7           58228           38971           31338
v  k                    9.2124e-09          1.8992        0.028649        0.025332
v  epsilon              1.8454e-06      1.3972e+05          203.36          17.057
v  TurbVisc             6.0725e-14         0.22693       0.0030465        0.014552
v  CourantNb             0.0064277      1.2011e+05          175.65          39.186
v  FourierNb               0.22421      2.3653e+06          219.33           3.015
v  total_pressure       4.9434e+05      5.5823e+05      5.3897e+05      5.3134e+05
v  Local Time Step            0.01         0.15698        0.010002        0.010021


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.634      2.3743e+06          394.98          42.201


 TIME FOR THE TIME STEP              394:        0.16690E+03

===============================================================


 INSTANT    0.395000000E+02   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        -0.177674597E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444383E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57382E+01 0.29972E+01
   Friction velocity        uet   :  0.32981E-01 0.37594E+02
   Friction velocity        uk    :  0.32459E-01 0.37594E+02
   Dimensionless distance   yplus :  0.24969E-02 0.12410E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6232
   Nb of faces within the viscous sub-layer     :      19397
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13521E+01     464   0.23039E+00   0.82546E+00 0.24545E+01 
c  Velocity[X]                                      0.26999E+00 
c  Velocity[Y]                                      0.34544E+00 
c  Velocity[Z]                                      0.21003E+00 
c  Pressure     0.37780E-01     672   0.76101E-02   0.24251E-01 0.11083E-01 
c  k            0.59590E-01     272   0.29328E-03   0.11480E-03 0.21281E+01 
c  epsilon      0.66171E+03     123   0.30997E-03   0.15184E+05 0.75027E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.4726e-05                             3
a  epsilon                -0.45408                            13
a  Local Time Step      4.2278e-08                        281748


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2333          7.6974         0.81356         0.18599
v  Velocity[Y]             -6.4838          10.611         0.62383         0.43669
v  Velocity[Z]             -9.7367            6.27        -0.49186      -0.0057847
v  ǁVelocityǁ            0.0050099          11.774          2.9334            3.56
v  Pressure                -5660.1           58231           38973           31339
v  k                    1.6121e-08            1.88        0.028724         0.02534
v  epsilon              0.00067605      1.3759e+05          203.59          17.049
v  TurbVisc              5.379e-14          0.2285       0.0030477        0.014555
v  CourantNb              0.039807      1.2052e+05          175.67          39.175
v  FourierNb               0.22421      2.3653e+06          219.33          3.0153
v  total_pressure       4.9434e+05      5.5823e+05      5.3897e+05      5.3134e+05
v  Local Time Step            0.01         0.15699        0.010002        0.010021


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6335      2.3723e+06             395           42.19


 TIME FOR THE TIME STEP              395:        0.15259E+03

===============================================================


 INSTANT    0.396000000E+02   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        -0.127300661E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444380E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57779E+01 0.29791E+01
   Friction velocity        uet   :  0.27006E-01 0.28037E+02
   Friction velocity        uk    :  0.26997E-01 0.28037E+02
   Dimensionless distance   yplus :  0.29029E-02 0.12410E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6265
   Nb of faces within the viscous sub-layer     :      19382
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13529E+01     517   0.22551E+00   0.85061E+00 0.24916E+01 
c  Velocity[X]                                      0.29876E+00 
c  Velocity[Y]                                      0.33158E+00 
c  Velocity[Z]                                      0.22027E+00 
c  Pressure     0.37900E-01     773   0.75541E-02   0.24320E-01 0.13307E-01 
c  k            0.59625E-01     270   0.41615E-03   0.14494E-03 0.23847E+01 
c  epsilon      0.66233E+03     129   0.28974E-03   0.14123E+05 0.72284E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00034333                             8
a  epsilon                 -2.4502                            17
a  Local Time Step      4.2278e-08                        281747


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -4.242          7.7233         0.81542          0.1859
v  Velocity[Y]             -6.4636           10.78         0.62469         0.43667
v  Velocity[Z]             -9.9256          6.1346        -0.49393      -0.0058196
v  ǁVelocityǁ            0.0060438          12.086           2.931          3.5599
v  Pressure                -5669.6           58229           38969           31336
v  k                    1.6118e-08          1.8992        0.028776        0.025365
v  epsilon              0.00065261      1.3919e+05          203.36           17.08
v  TurbVisc             8.2139e-14         0.22982       0.0030675        0.014561
v  CourantNb              0.015689      1.2085e+05          175.96          39.194
v  FourierNb               0.22418      2.3653e+06          219.34          3.0168
v  total_pressure       4.9433e+05      5.5823e+05      5.3897e+05      5.3134e+05
v  Local Time Step            0.01         0.15699        0.010002        0.010023


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6498      2.3765e+06           395.3          42.211


 TIME FOR THE TIME STEP              396:        0.15872E+03

===============================================================


 INSTANT    0.397000000E+02   TIME STEP NUMBER             397
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
----------------------------------------------Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444381E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57680E+01 0.29831E+01
   Friction velocity        uet   :  0.24822E-01 0.35070E+02
   Friction velocity        uk    :  0.30520E-01 0.35070E+02
   Dimensionless distance   yplus :  0.29225E-02 0.12427E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6257
   Nb of faces within the viscous sub-layer     :      19395
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13534E+01     463   0.22883E+00   0.86631E+00 0.25150E+01 
c  Velocity[X]                                      0.30205E+00 
c  Velocity[Y]                                      0.34375E+00 
c  Velocity[Z]                                      0.22050E+00 
c  Pressure     0.37686E-01     518   0.75924E-02   0.24190E-01 0.13120E-01 
c  k            0.59630E-01     269   0.30749E-03   0.12012E-03 0.21784E+01 
c  epsilon      0.66452E+03     114   0.24003E-03   0.10303E+05 0.61574E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -2.344e-05                             3
a  epsilon                -0.21607                             5
a  Local Time Step      4.2278e-08                        281747


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2525          7.7147         0.81436         0.18586
v  Velocity[Y]             -6.4751          10.809         0.62233          0.4368
v  Velocity[Z]             -9.8613          6.3608        -0.48961      -0.0059937
v  ǁVelocityǁ            0.0022812          12.082          2.9322          3.5595
v  Pressure                -5677.5           58236           38975           31339
v  k                    1.8389e-08          1.9042        0.028671        0.025343
v  epsilon              0.00071696      1.4013e+05          203.66           17.06
v  TurbVisc             1.2594e-14         0.23041       0.0030725        0.014565
v  CourantNb               0.11939      1.1487e+05           175.6          39.181
v  FourierNb               0.22413      2.3653e+06          219.32          3.0177
v  total_pressure       4.9432e+05      5.5824e+05      5.3897e+05      5.3134e+05
v  Local Time Step            0.01         0.17304        0.010002        0.010022


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6598      2.3752e+06          394.92          42.199


 TIME FOR THE TIME STEP              398:        0.14651E+03

===============================================================


 INSTANT    0.399000000E+02   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         0.131980976E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444501E+01
Free inlet               13           0         0.000000000E+00
Convective inlet  Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444381E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57680E+01 0.29831E+01
   Friction velocity        uet   :  0.24822E-01 0.35070E+02
   Friction velocity        uk    :  0.30520E-01 0.35070E+02
   Dimensionless distance   yplus :  0.29225E-02 0.12427E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6257
   Nb of faces within the viscous sub-layer     :      19395
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13534E+01     463   0.22883E+00   0.86631E+00 0.25150E+01 
c  Velocity[X]                                      0.30205E+00 
c  Velocity[Y]                                      0.34375E+00 
c  Velocity[Z]                                      0.22050E+00 
c  Pressure     0.37686E-01     518   0.75924E-02   0.24190E-01 0.13120E-01 
c  k            0.59630E-01     269   0.30749E-03   0.12012E-03 0.21784E+01 
c  epsilon      0.66452E+03     114   0.24003E-03   0.10303E+05 0.61574E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -2.344e-05                             3
a  epsilon                -0.21607                             5
a  Local Time Step      4.2278e-08                        281747


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2525          7.7147         0.81436         0.18586
v  Velocity[Y]             -6.4751          10.809         0.62233          0.4368
v  Velocity[Z]             -9.8613          6.3608        -0.48961      -0.0059937
v  ǁVelocityǁ            0.0022812          12.082          2.9322          3.5595
v  Pressure                -5677.5           58236           38975           31339
v  k                    1.8389e-08          1.9042        0.028671        0.025343
v  epsilon              0.00071696      1.4013e+05          203.66           17.06
v  TurbVisc             1.2594e-14         0.23041       0.0030725        0.014565
v  CourantNb               0.11939      1.1487e+05           175.6          39.181
v  FourierNb               0.22413      2.3653e+06          219.32          3.0177
v  total_pressure       4.9432e+05      5.5824e+05      5.3897e+05      5.3134e+05
v  Local Time Step            0.01         0.17304        0.010002        0.010022


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6598      2.3752e+06          394.92          42.199


 TIME FOR THE TIME STEP              398:        0.14945E+03

===============================================================


 INSTANT    0.399000000E+02   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         0.131980976E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444501E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57159E+01 0.29959E+01
   Friction velocity        uet   :  0.22026E-01 0.18796E+02
   Friction velocity        uk    :  0.21637E-01 0.18796E+02
   Dimensionless distance   yplus :  0.15599E-02 0.12421E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6238
   Nb of faces within the viscous sub-layer     :      19361
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13515E+01     522   0.23079E+00   0.92944E+00 0.26045E+01 
c  Velocity[X]                                      0.31502E+00 
c  Velocity[Y]                                      0.37434E+00 
c  Velocity[Z]                                      0.24009E+00 
c  Pressure     0.38259E-01     632   0.78002E-02   0.24561E-01 0.12387E-01 
c  k            0.59623E-01     303   0.41733E-03   0.17271E-03 0.26106E+01 
c  epsilon      0.66249E+03     148   0.29961E-03   0.17055E+05 0.79586E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00026093                             8
a  epsilon                 -4.5634                            27
a  Local Time Step      4.2278e-08                        281739


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2338          7.7195         0.81508         0.18569
v  Velocity[Y]             -6.4933          10.562         0.62216          0.4367
v  Velocity[Z]             -9.7772          5.9831        -0.49308      -0.0058273
v  ǁVelocityǁ            0.0057324          11.761          2.9275          3.5601
v  Pressure                -5683.6           58233           38973           31338
v  k                    1.8693e-08          1.8886        0.028795        0.025348
v  epsilon              0.00069049      1.3837e+05          203.36          17.075
v  TurbVisc             9.7774e-14         0.23487       0.0030896        0.014567
v  CourantNb             0.0063345      1.1652e+05          175.69          39.178
v  FourierNb               0.22413      2.3653e+06          219.36          3.0175
v  total_pressure       4.9432e+05      5.5823e+05      5.3897e+05      5.3134e+05
v  Local Time Step            0.01         0.17304        0.010002        0.010016


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6729       2.374e+06          395.05          42.196


 TIME FOR THE TIME STEP              399:        0.16662E+03

===============================================================


 INSTANT    0.400000000E+02   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        -0.114721477E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444503E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57390E+01 0.29923E+01
   Friction velocity        uet   :  0.32573E-01 0.38151E+02
   Friction velocity        uk    :  0.34946E-01 0.38151E+02
   Dimensionless distance   yplus :  0.21492E-02 0.12407E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6266
   Nb of faces within the viscous sub-layer     :      19385
   Total number of wall faces                   :      41000
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration        400, Physical time    0.40000E+02


   ** Writing the main restart file
      -----------------------------

 Start writing
  Wrote field names and types to checkpoint: checkpoint/main
   End writing the options                              
  Wrote main    ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6227
   Nb of faces within the viscous sub-layer     :      19394
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16489E+01     619   0.18330E+00   0.10740E+03 0.22299E+02 
c  Velocity[X]                                      0.42191E+01 
c  Velocity[Y]                                      0.84278E+01 
c  Velocity[Z]                                      0.94750E+02 
c  Pressure     0.43080E-01    1863   0.18559E+00   0.27641E-01 0.36541E+02 
c  k            0.15317E+00     290   0.18508E-02   0.15518E+00 0.47445E+02 
c  epsilon      0.66132E+03     162   0.39753E-03   0.20818E+05 0.89765E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -6.515e-05                             5
a  epsilon                 -1.1907                            18
a  Local Time Step      4.2278e-08                        281746


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.1973          11.039         0.99268         0.24319
v  Velocity[Y]             -8.7487          14.403         0.84547         0.56157
v  Velocity[Z]             -14.162          7.6282        -0.53299        0.025355
v  ǁVelocityǁ            0.0041895          18.054          3.3531          4.4721
v  Pressure                  0.638           92685           59776           51549
v  k                    2.0638e-08          1.8489        0.028469        0.038863
v  epsilon              0.00075011      1.3571e+05          209.48          18.724
v  TurbVisc             5.3475e-14         0.23035       0.0030178        0.014558
v  CourantNb               0.14521      1.0505e+05          175.34           39.17
v  FourierNb               0.22421      2.3653e+06          219.25          3.0143
v  total_pressure            5e+05      5.9269e+05      5.5978e+05      5.5155e+05
v  Local Time Step            0.01         0.17304        0.010002        0.010017


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6289      2.3769e+06          394.59          42.184


 TIME FOR THE TIME STEP              401:        0.21749E+03

===============================================================


 INSTANT    0.402000000E+02   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         0.600309152E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245779E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10212E+02 0.36375E+01
   Friction velocity        uet   :  0.24803E-01 0.33482E+02
   Friction velocity        uk    :  0.24327E-01 0.33482E+02
   Dimensionless distance   yplus :  0.25079E-02 0.15285E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7567
   Nb of faces within the viscous sub-layer     :      18055
   Total number of wall faces    ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6227
   Nb of faces within the viscous sub-layer     :      19394
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16489E+01     619   0.18330E+00   0.10740E+03 0.22299E+02 
c  Velocity[X]                                      0.42191E+01 
c  Velocity[Y]                                      0.84278E+01 
c  Velocity[Z]                                      0.94750E+02 
c  Pressure     0.43080E-01    1863   0.18559E+00   0.27641E-01 0.36541E+02 
c  k            0.15317E+00     290   0.18508E-02   0.15518E+00 0.47445E+02 
c  epsilon      0.66132E+03     162   0.39753E-03   0.20818E+05 0.89765E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -6.515e-05                             5
a  epsilon                 -1.1907                            18
a  Local Time Step      4.2278e-08                        281746


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.1973          11.039         0.99268         0.24319
v  Velocity[Y]             -8.7487          14.403         0.84547         0.56157
v  Velocity[Z]             -14.162          7.6282        -0.53299        0.025355
v  ǁVelocityǁ            0.0041895          18.054          3.3531          4.4721
v  Pressure                  0.638           92685           59776           51549
v  k                    2.0638e-08          1.8489        0.028469        0.038863
v  epsilon              0.00075011      1.3571e+05          209.48          18.724
v  TurbVisc             5.3475e-14         0.23035       0.0030178        0.014558
v  CourantNb               0.14521      1.0505e+05          175.34           39.17
v  FourierNb               0.22421      2.3653e+06          219.25          3.0143
v  total_pressure            5e+05      5.9269e+05      5.5978e+05      5.5155e+05
v  Local Time Step            0.01         0.17304        0.010002        0.010017


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6289      2.3769e+06          394.59 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.350832171E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245793E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11127E+02 0.35989E+01
   Friction velocity        uet   :  0.31214E-01 0.56318E+02
   Friction velocity        uk    :  0.45862E-01 0.56318E+02
   Dimensionless distance   yplus :  0.71862E-02 0.16274E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7620
   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     0.23916E+01     688   0.20833E+00   0.97555E+01 0.61788E+01 
c  Velocity[X]                                      0.23458E+01 
c  Velocity[Y]                                      0.37259E+01 
c  Velocity[Z]                                      0.36838E+01 
c  Pressure     0.29584E+00    1502   0.14232E+00   0.17870E+00 0.54242E+01 
c  k            0.16372E+00     231   0.11389E-02   0.12654E-01 0.12365E+02 
c  epsilon      0.15507E+04     123   0.41235E-02   0.60614E+07 0.11218E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0042666                           221
a  epsilon                 -738.28                           418
a  Local Time Step      2.9595e-08                        281770


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2585          11.746          1.0158         0.26742
v  Velocity[Y]             -7.5397          14.687         0.99048         0.63509
v  Velocity[Z]             -13.482          9.5284        -0.43799        0.088059
v  ǁVelocityǁ             0.030623          18.525          3.4941          4.8956
v  Pressure                -99.272           90448           64793           51784
v  k                    1.0874e-08          1.9013        0.028258        0.046251
v  epsilon               8.426e-05      1.5379e+05          311.19          23.738
v  TurbVisc             9.2081e-14         0.32674       0.0025105        0.025389
v  CourantNb              0.029753      3.3789e+05          223.04          51.253
v  FourierNb               0.22515      2.3653e+06          218.48          3.1071
v  total_pressure        4.999e+05      5.9045e+05      5.6479e+05      5.5178e+05
v  Local Time Step            0.01        0.021612            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2136      2.7032e+06          441.52           54.36


 TIME FOR THE TIME STEP              403:        0.21533E+03

===============================================================


 INSTANT    0.404000000E+02   TIME STEP NUMBER             404
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Bou ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.350832171E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245793E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11127E+02 0.35989E+01
   Friction velocity        uet   :  0.31214E-01 0.56318E+02
   Friction velocity        uk    :  0.45862E-01 0.56318E+02
   Dimensionless distance   yplus :  0.71862E-02 0.16274E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7620
   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     0.23916E+01     688   0.20833E+00   0.97555E+01 0.61788E+01 
c  Velocity[X]                                      0.23458E+01 
c  Velocity[Y]                                      0.37259E+01 
c  Velocity[Z]                                      0.36838E+01 
c  Pressure     0.29584E+00    1502   0.14232E+00   0.17870E+00 0.54242E+01 
c  k            0.16372E+00     231   0.11389E-02   0.12654E-01 0.12365E+02 
c  epsilon      0.15507E+04     123   0.41235E-02   0.60614E+07 0.11218E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0042666                           221
a  epsilon                 -738.28                           418
a  Local Time Step      2.9595e-08                        281770


  ** Computed fiev  Velocity[X]             -4.4373          11.807          1.0142         0.25975
v  Velocity[Y]              -7.323          14.148           1.012         0.62415
v  Velocity[Z]             -12.513          9.1965         -0.5599        0.011803
v  ǁVelocityǁ             0.019166          17.471          3.5532           4.909
v  Pressure                -1403.8           88480           61352           47977
v  k                    7.7998e-09          2.5911        0.029934        0.046278
v  epsilon              3.8658e-05      4.1379e+05          401.85          24.839
v  TurbVisc             5.0089e-14         0.32654       0.0020278        0.025885
v  CourantNb              0.044495      2.4116e+05          223.33          51.498
v  FourierNb                0.2249      2.3653e+06          218.11          3.0838
v  total_pressure        4.986e+05      5.8848e+05      5.6135e+05      5.4798e+05
v  Local Time Step            0.01        0.022562            0.01        0.010001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.87328      2.6065e+06          441.44          54.582


 TIME FOR THE TIME STEP              404:        0.21750E+03

===============================================================


 INSTANT    0.405000000E+02   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        -0.645209641E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245925E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.91455E+01 0.36025E+01
   Friction velocity        uet   :  0.30540E-01 0.54383E+02
   Friction velocity        uk    :  0.35832E-01 0.54383E+02
   Dimensionless distance   yplus :  0.51943E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7995
   Nb of faces within the viscous sub-layer     :      16929
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23513E+01     614   0.20439E+00   0.58555E+01 0.47804E+01 
c  Velocity[X]                                      0.11393E+01 
c  Velocity[Y]                                      0.19657E+01 
c  Velocity[Z]                                      0.27505E+01 
c  Pressure     0.27673E+00    1609   0.10750E+00   0.15854E+00 0.50826E+01 
c  k            0.16354E+00     214   0.29287E-03   0.28514E-02 0.59072E+01 
c  epsilon      0.14172E+04     109   0.14330E-02   0.97928E+06 0.42773E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0014374                            76
a  epsilon                 -712.83                           144
a  Local Time Step      4.2278e-08                        281777


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.4673          11.419           1.017         0.25447
v  Velocity[Y]             -7.1028          14.419          1.0108         0.61315
v  Velocity[Z]              -12.64          v  Velocity[X]             -4.4373          11.807          1.0142         0.25975
v  Velocity[Y]              -7.323          14.148           1.012         0.62415
v  Velocity[Z]             -12.513          9.1965         -0.5599        0.011803
v  ǁVelocityǁ             0.019166          17.471          3.5532           4.909
v  Pressure                -1403.8           88480           61352           47977
v  k                    7.7998e-09          2.5911        0.029934        0.046278
v  epsilon              3.8658e-05      4.1379e+05          401.85          24.839
v  TurbVisc             5.0089e-14         0.32654       0.0020278        0.025885
v  CourantNb              0.044495      2.4116e+05          223.33          51.498
v  FourierNb                0.2249      2.3653e+06          218.11          3.0838
v  total_pressure        4.986e+05      5.8848e+05      5.6135e+05      5.4798e+05
v  Local Time Step            0.01        0.022562            0.01        0.010001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.87328      2.6065e+06          441.44          54.582


 TIME FOR THE TIME STEP              404:        0.21150E+03

===============================================================


 INSTANT    0.405000000E+02   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        -0.645209641E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245925E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.91455E+01 0.36025E+01
   Friction velocity        uet   :  0.30540E-01 0.54383E+02
   Friction velocity        uk    :  0.35832E-01 0.54383E+02
   Dimensionless distance   yplus :  0.51943E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7995
   Nb of faces within the viscous sub-layer     :      16929
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23513E+01     614   0.20439E+00   0.58555E+01 0.47804E+01 
c  Velocity[X]                                      0.11393E+01 
c  Velocity[Y]                                      0.19657E+01 
c  Velocity[Z]                                      0.27505E+01 
c  Pressure     0.27673E+00    1609   0.10750E+00   0.15854E+00 0.50826E+01 
c  k            0.16354E+00     214   0.29287E-03   0.28514E-02 0.59072E+01 
c  epsilon      0.14172E+04     109   0.14330E-02   0.97928E+06 0.42773E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0014374                            76
a  epsilon                 -712.83                           144
a  Local Time Step      4.2278e-08                        281777


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.4673          11.419           1.017         0.25447
v  Velocity[Y]             -7.1028          14.419          1.0108         0.61315
v  Velocity[Z]              -12.64          8.6181         -0.6463       -0.026374
v  ǁVelocityǁ            0.0094969          16.645          3.6158          4.9006
v  Pressure                -6588.3           86214           58223           45297
v  k                    9.4008e-09          1.9159        0.028492        0.046094
v  epsilon              0.00025986      1.6034e+05          354.46          24.411
v  TurbVisc             2.8595e-14          0.3266       0.0018034         0.02613
v  CourantNb            0.00072258      2.2668e+05          221.57          51.785
v  FourierNb               0.22464      2.3653e+06          218.01          3.0691
v  total_pressure       4.9341e+05      5.8621e+05      5.5822e+05       5.453e+05
v  Local Time Step            0.01        0.024818            0.01        0.010001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.91051       2.592e+06          439.58          54.855


 TIME FOR THE TIME STEP              405:        0.20837E+03

===============================================================


 INSTANT    0.406000000E+02   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        -0.909810252E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245937E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.87790E+01 0.36019E+01
   Friction velocity        uet   :  0.33556E-01 0.55528E+02
   Friction velocity        uk    :  0.38486E-01 0.55528E+02
   Dimensionless distance   yplus :  0.70855E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8073
   Nb of faces within the viscous sub-layer     :      16779
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23315E+01     622   0.20366E+00   0.44367E+01 0.41712E+01 
c  Velocity[X]                                      0.10265E+01 
c  Velocity[Y]                                      0.16082E+01 
c  Velocity[Z]                                      0.18020E+01 
c  Pressure     0.24644E+00    1470   0.92414E-01   0.13744E+00 0.19601E+01 
c  k            0.16347E+00     209   0.21507E-03   0.13979E-02 0.41406E+01 
c  epsilon      0.13566E+04     127   0.73692E-03   0.27977E+06 0.22167E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0014742                            34
a  epsilon                 -3.6904                            75
a  Local Time Step      4.2278e-08                        281771


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.5742           10.09          1.0226         0.25275
v  Velocity[Y]             -7.0208          14.196         0.99768         0.60792
v  Velocity[Z]             -12.574          8.4279        -0.67876       -0.028612
v  ǁVelocityǁ            0.0076221          16.175          3.6569          4.8866
v  Pressure                -9440.6           85510           56898           44550
v  k                    1.6297e-08          1.9618        0.029578        0.045979
v  epsilon              0.00025934       1.632e+05          377.06            24.7
v  TurbVisc             5.5189e-14         0.32657       0.0017306        0.026195
v  CourantNb              0.067027      1.4875e+05          222.52          52.077
v  FourierNb               0.22468      2.3653e+06          217.98          3.0625
v  total_pressure       4.9056e+05      5.8551e+05       5.569e+05      5.4455e+05
v  Local Time Step            0.01          0.0273            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.9368       2.486e+06           440.5           55.14


 TIME FOR THE TIME STEP              406:        0.20210E+03

===============================================================


 INSTANT    0.407000000E+02   TIME STEP NUMBER             407
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ----------Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.931828561E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245778E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.86011E+01 0.36013E+01
   Friction velocity        uet   :  0.30000E-01 0.46446E+02
   Friction velocity        uk    :  0.29964E-01 0.46446E+02
   Dimensionless distance   yplus :  0.59265E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8184
   Nb of faces within the viscous sub-layer     :      16665
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23260E+01     610   0.20399E+00   0.28451E+01 0.33446E+01 
c  Velocity[X]                                      0.69657E+00 
c  Velocity[Y]                                      0.11607E+01 
c  Velocity[Z]                                      0.98787E+00 
c  Pressure     0.20610E+00    1483   0.73886E-01   0.10891E+00 0.30199E+01 
c  k            0.16334E+00     195   0.23050E-03   0.12123E-02 0.38648E+01 
c  epsilon      0.12755E+04     103   0.67918E-03   0.28303E+06 0.21850E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00067558                            21
a  epsilon                 -80.917                            60
a  Local Time Step      4.2278e-08                        281763


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.6213          9.0445          1.0468         0.25663
v  Velocity[Y]             -7.1458          14.759         0.94385         0.61082
v  Velocity[Z]             -12.533          8.1706        -0.63196      -0.0071474
v  ǁVelocityǁ            0.0046346          16.665          3.6932          4.8784
v  Pressure                -9974.7           88670           58870           47083
v  k                    1.9285e-08            1.98        0.029657        0.045673
v  epsilon              0.00010906      1.8247e+05          384.88           24.75
v  TurbVisc             6.1282e-14         0.32657       0.0017655        0.026219
v  CourantNb              0.041587      1.2599e+05          224.14          52.447
v  FourierNb               0.22465      2.3653e+06          218.19           3.059
v  total_pressure       4.9003e+05      5.8867e+05      5.5887e+05      5.4708e+05
v  Local Time Step            0.01        0.033033            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0774      2.4484e+06          442.33          55.506


 TIME FOR THE TIME STEP              408:        0.19762E+03

===============================================================


 INSTANT    0.409000000E+02   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         0.144161715E-17
Rough wall                6           0         0.000000000E+00
Symmetry          Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.931828561E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245778E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.86011E+01 0.36013E+01
   Friction velocity        uet   :  0.30000E-01 0.46446E+02
   Friction velocity        uk    :  0.29964E-01 0.46446E+02
   Dimensionless distance   yplus :  0.59265E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8184
   Nb of faces within the viscous sub-layer     :      16665
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23260E+01     610   0.20399E+00   0.28451E+01 0.33446E+01 
c  Velocity[X]                                      0.69657E+00 
c  Velocity[Y]                                      0.11607E+01 
c  Velocity[Z]                                      0.98787E+00 
c  Pressure     0.20610E+00    1483   0.73886E-01   0.10891E+00 0.30199E+01 
c  k            0.16334E+00     195   0.23050E-03   0.12123E-02 0.38648E+01 
c  epsilon      0.12755E+04     103   0.67918E-03   0.28303E+06 0.21850E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00067558                            21
a  epsilon                 -80.917                            60
a  Local Time Step      4.2278e-08                        281763


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.6213          9.0445          1.0468         0.25663
v  Velocity[Y]             -7.1458       v  Pressure                -9406.3           90873           60497           48721
v  k                    2.7264e-08          2.0014        0.029635        0.045589
v  epsilon               0.0002241       1.703e+05          384.87          24.783
v  TurbVisc             1.2835e-13         0.39601       0.0016969        0.026203
v  CourantNb               0.10871      1.3923e+05          225.67          52.616
v  FourierNb               0.22466      2.3653e+06          218.22          3.0533
v  total_pressure       4.9059e+05      5.9087e+05       5.605e+05      5.4872e+05
v  Local Time Step            0.01        0.036336            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.3282      2.4389e+06          443.89          55.669


 TIME FOR THE TIME STEP              409:        0.20031E+03

===============================================================


 INSTANT    0.410000000E+02   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         0.540098857E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245763E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.85740E+01 0.36008E+01
   Friction velocity        uet   :  0.32708E-01 0.38211E+02
   Friction velocity        uk    :  0.42498E-01 0.38211E+02
   Dimensionless distance   yplus :  0.43026E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8261
   Nb of faces within the viscous sub-layer     :      16592
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23411E+01     598   0.20713E+00   0.25260E+01 0.31357E+01 
c  Velocity[X]                                      0.67721E+00 
c  Velocity[Y]                                      0.11413E+01 
c  Velocity[Z]                                      0.70745E+00 
c  Pressure     0.18285E+00    1477   0.59772E-01   0.91646E-01 0.22558E+01 
c  k            0.16324E+00     176   0.12507E-03   0.41001E-03 0.22484E+01 
c  epsilon      0.12061E+04     106   0.62447E-03   0.17002E+06 0.16892E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0003678                            21
a  epsilon                 -15.956                            58
a  Local Time Step      4.2278e-08                        281771


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.6548          8.9427          1.0598         0.25981
v  Velocity[Y]             -7.2575          14.241         0.90281         0.61585
v  Velocity[Z]             -12.404          7.9972        -0.59622      -0.0025155
v  ǁVelocityǁ             0.018086          15.996          3.7334          4.9004
v  Pressure                -9035.7           92722           61812           49963
v  k                    3.0848e-08          2.0344        0.029756        0.045545
v  epsilon               0.0010983      1.75v  Pressure                -9406.3           90873           60497           48721
v  k                    2.7264e-08          2.0014        0.029635        0.045589
v  epsilon               0.0002241       1.703e+05          384.87          24.783
v  TurbVisc             1.2835e-13         0.39601       0.0016969        0.026203
v  CourantNb               0.10871      1.3923e+05          225.67          52.616
v  FourierNb               0.22466      2.3653e+06          218.22          3.0533
v  total_pressure       4.9059e+05      5.9087e+05       5.605e+05      5.4872e+05
v  Local Time Step            0.01        0.036336            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.3282      2.4389e+06          443.89          55.669


 TIME FOR THE TIME STEP              409:        0.19543E+03

===============================================================


 INSTANT    0.410000000E+02   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         0.540098857E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245763E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.85740E+01 0.36008E+01
   Friction velocity        uet   :  0.32708E-01 0.38211E+02
   Friction velocity        uk    :  0.42498E-01 0.38211E+02
   Dimensionless distance   yplus :  0.43026E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8261
   Nb of faces within the viscous sub-layer     :      16592
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23411E+01     598   0.20713E+00   0.25260E+01 0.31357E+01 
c  Velocity[X]                                      0.67721E+00 
c  Velocity[Y]                                      0.11413E+01 
c  Velocity[Z]                                      0.70745E+00 
c  Pressure     0.18285E+00    1477   0.59772E-01   0.91646E-01 0.22558E+01 
c  k            0.16324E+00     176   0.12507E-03   0.41001E-03 0.22484E+01 
c  epsilon      0.12061E+04     106   0.62447E-03   0.17002E+06 0.16892E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0003678                            21
a  epsilon                 -15.956                            58
a  Local Time Step      4.2278e-08                        281771


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.6548          8.9427          1.0598         0.25981
v  Velocity[Y]             -7.2575          14.241         0.90281         0.61585
v  Velocity[Z]             -12.404          7.9972        -0.59622      -0.0025155
v  ǁVelocityǁ             0.018086          15.996          3.7334          4.9004
v  Pressure                -9035.7           92722           61812           49963
v  k                    3.0848e-08          2.0344        0.029756        0.045545
v  epsilon               0.0010983      1.7569e+05          389.33          24.841
v  TurbVisc             1.5289e-13         0.32657       0.0016687        0.026194
v  CourantNb             0.0031644      1.5789e+05          226.76          52.791
v  FourierNb               0.22473      2.3653e+06          218.28          3.0501
v  total_pressure       4.9096e+05      5.9272e+05      5.6181e+05      5.4996e+05
v  Local Time Step            0.01         0.03997            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5956      2.4243e+06          445.04          55.841


 TIME FOR THE TIME STEP              410:        0.19499E+03

===============================================================


 INSTANT    0.411000000E+02   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         0.220653680E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245779E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.85751E+01 0.35998E+01
   Friction velocity        uet   :  0.31248E-01 0.39695E+02
   Friction velocity        uk    :  0.35750E-01 0.39695E+02
   Dimensionless distance   yplus :  0.29514E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8293
   Nb of faces within the viscous sub-layer     :      16561
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23507E+01     599   0.21154E+00   0.25965E+01 0.31700E+01 
c  Velocity[X]                                      0.69181E+00 
c  Velocity[Y]                                      0.11451E+01 
c  Velocity[Z]                                      0.75965E+00 
c  Pressure     0.17574E+00    1410   0.53761E-01   0.85908E-01 0.15282E+01 
c  k            0.16322E+00     162   0.19503E-03   0.34188E-03 0.20528E+01 
c  epsilon      0.11921E+04      98   0.68919E-03   0.15967E+06 0.16230E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00098978                            12
a  epsilon                 -9.7523                            21
a  Local Time Step      4.2278e-08                        281772


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.6888          9.0531          1.0688         0.26034
v  Velocity[Y]             -7.3443          13.773         0.88317         0.61726
v  Velocity[Z]             -12.492          8.1264        -0.58837      -0.0051634
v  ǁVelocityǁ             0.019453          15.457           3.757          4.9133
v  Pressure                -8951.3           94092           62715           50750
v  k                    9.7315e-09          2.0269         0.02969        0.045524
v  epsilon              0.00099432      1.7483e+05          392.99           24.88
v  TurbVisc             1.7641e-13         0.32658        0.001637         0.02619
v  CourantNb            0.00053746      1.5185e+05          226.87           52.93
v  FourierNb               0.22486      2.3653e+06          218.22          3.0484
v  total_pressure       4.9105e+05      5.9409e+05      5.6272e+05      5.5075e+05
v  Local Time Step            0.01        0.033191            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6652      2.4185e+06          445.08          55.978


 TIME FOR THE TIME STEP              411:        0.19206E+03

===============================================================


 INSTANT    0.412000000E+02   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       Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.87672E+01 0.35989E+01
   Friction velocity        uet   :  0.29811E-01 0.46646E+02
   Friction velocity        uk    :  0.50530E-01 0.46646E+02
   Dimensionless distance   yplus :  0.14159E-02 0.16022E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8343
   Nb of faces within the viscous sub-layer     :      16504
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23628E+01     576   0.21141E+00   0.23741E+01 0.30163E+01 
c  Velocity[X]                                      0.66460E+00 
c  Velocity[Y]                                      0.96324E+00 
c  Velocity[Z]                                      0.74623E+00 
c  Pressure     0.16145E+00    1297   0.45390E-01   0.75427E-01 0.73768E+00 
c  k            0.16321E+00     152   0.19740E-03   0.26953E-03 0.18223E+01 
c  epsilon      0.11653E+04      89   0.60994E-03   0.13105E+06 0.14425E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00017809                            44
a  epsilon                 -5.6088                            43
a  Local Time Step      4.2278e-08                        281773


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.7563            9.36          1.0801         0.26057
v  Velocity[Y]             -7.6469          14.406         0.86862         0.61885
v  Velocity[Z]             -12.301          8.7216        -0.59577       -0.010399
v  ǁVelocityǁ            0.0077989          15.964           3.798          4.9345
v  Pressure                -9440.9           95704           63621           51374
v  k                    2.0838e-09           2.052        0.029967        0.045543
v  epsilon              3.2874e-05       1.824e+05          403.26          25.105
v  TurbVisc             3.4469e-13         0.32658       0.0015883        0.026185
v  CourantNb               0.24078      1.5899e+05          229.11          53.251
v  FourierNb               0.22483      2.3653e+06          218.06          3.0468
v  total_pressure       4.9056e+05       5.957e+05      5.6362e+05      5.5137e+05
v  Local Time Step            0.01        0.023579            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5846      2.3891e+06          447.17          56.297


 TIME FOR THE TIME STEP              413:        0.18842E+03

===============================================================


 INSTANT    0.414000000E+02   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        -0.237898021E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245770E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined         Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.87672E+01 0.35989E+01
   Friction velocity        uet   :  0.29811E-01 0.46646E+02
   Friction velocity        uk    :  0.50530E-01 0.46646E+02
   Dimensionless distance   yplus :  0.14159E-02 0.16022E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8343
   Nb of faces within the viscous sub-layer     :      16504
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23628E+01     576   0.21141E+00   0.23741E+01 0.30163E+01 
c  Velocity[X]                                      0.66460E+00 
c  Velocity[Y]                                      0.96324E+00 
c  Velocity[Z]                                      0.74623E+00 
c  Pressure     0.16145E+00    1297   0.45390E-01   0.75427E-01 0.73768E+00 
c  k            0.16321E+00     152   0.19740E-03   0.26953E-03 0.18223E+01 
c  epsilon      0.11653E+04      89   0.60994E-03   0.13105E+06 0.14425E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00017809                            44
a  epsilon                 -5.6088                            43
a  Local Time Step      4.2278e-08                        281773


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.7563            9.36          1.0801         0.26057
v  Velocity[Y]             -7.6469          14.406         0.86862         0.61885
v  Velocity[Z]             -12.301          8.7216        -0.59577       -0.010399
v  ǁVelocityǁ            0.0077989          15.964           3.798          4.9345
v  Pressure                -9440.9           95704           63621           51374
v  k                    2.0838e-09     v  CourantNb             0.0098085      1.5273e+05           229.9          53.372
v  FourierNb               0.22468      2.3653e+06          218.03          3.0469
v  total_pressure       4.9026e+05      5.9625e+05      5.6392e+05      5.5152e+05
v  Local Time Step            0.01        0.025937            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4095      2.3797e+06          447.93          56.419


 TIME FOR THE TIME STEP              414:        0.18153E+03

===============================================================


 INSTANT    0.415000000E+02   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        -0.246734186E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245765E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.90899E+01 0.35986E+01
   Friction velocity        uet   :  0.32767E-01 0.51184E+02
   Friction velocity        uk    :  0.35906E-01 0.51184E+02
   Dimensionless distance   yplus :  0.30041E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8427
   Nb of faces within the viscous sub-layer     :      16430
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23728E+01     558   0.22605E+00   0.25469E+01 0.31152E+01 
c  Velocity[X]                                      0.67577E+00 
c  Velocity[Y]                                      0.10396E+01 
c  Velocity[Z]                                      0.83150E+00 
c  Pressure     0.15303E+00    1265   0.40753E-01   0.69013E-01 0.64263E+00 
c  k            0.16326E+00     142   0.12752E-03   0.27454E-03 0.18384E+01 
c  epsilon      0.11881E+04     173   0.61740E-03   0.26045E+06 0.19424E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -3.2696                             3
a  Local Time Step      4.2278e-08                        281777


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.7484          9.5975          1.0937         0.26003
v  Velocity[Y]             -7.9031          14.405         0.85479         0.61853
v  Velocity[Z]             -12.657          8.7855        -0.61198       -0.011803
v  ǁVelocityǁ            0.0086567          15.963          3.8473          4.9468
v  Pressure                -9934.2           96792           64269           51700
v  k                    1.2223e-07          2.2016        0.030546        0.045583
v  epsilon               0.0028132      2.2675e+05          426.03          25.399
v  TurbVisc             5.1724e-13         0.32658       0.0015752        0.026182
v  CourantNb               0.13973      1.6589e+05          231.63          53.516
v  FourierNb               0.22443      2.3653e+06          218.04           3.046
v  total_pressure       4.9007e+05      5.9679e+05      5.6427e+05       5.517e+05
v  Locav  CourantNb             0.0098085      1.5273e+05           229.9          53.372
v  FourierNb               0.22468      2.3653e+06          218.03          3.0469
v  total_pressure       4.9026e+05      5.9625e+05      5.6392e+05      5.5152e+05
v  Local Time Step            0.01        0.025937            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4095      2.3797e+06          447.93          56.419


 TIME FOR THE TIME STEP              414:        0.18530E+03

===============================================================


 INSTANT    0.415000000E+02   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        -0.246734186E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245765E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.90899E+01 0.35986E+01
   Friction velocity        uet   :  0.32767E-01 0.51184E+02
   Friction velocity        uk    :  0.35906E-01 0.51184E+02
   Dimensionless distance   yplus :  0.30041E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8427
   Nb of faces within the viscous sub-layer     :      16430
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23728E+01     558   0.22605E+00   0.25469E+01 0.31152E+01 
c  Velocity[X]                                      0.67577E+00 
c  Velocity[Y]                                      0.10396E+01 
c  Velocity[Z]                                      0.83150E+00 
c  Pressure     0.15303E+00    1265   0.40753E-01   0.69013E-01 0.64263E+00 
c  k            0.16326E+00     142   0.12752E-03   0.27454E-03 0.18384E+01 
c  epsilon      0.11881E+04     173   0.61740E-03   0.26045E+06 0.19424E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -3.2696                             3
a  Local Time Step      4.2278e-08                        281777


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.7484          9.5975          1.0937         0.26003
v  Velocity[Y]             -7.9031          14.405         0.85479         0.61853
v  Velocity[Z]             -12.657          8.7855        -0.61198       -0.011803
v  ǁVelocityǁ            0.0086567          15.963          3.8473          4.9468
v  Pressure                -9934.2           96792           64269           51700
v  k                    1.2223e-07          2.2016        0.030546        0.045583
v  epsilon               0.0028132      2.2675e+05          426.03          25.399
v  TurbVisc             5.1724e-13         0.32658       0.0015752        0.026182
v  CourantNb               0.13973      1.6589e+05          231.63          53.516
v  FourierNb               0.22443      2.3653e+06          218.04           3.046
v  total_pressure       4.9007e+05      5.9679e+05      5.6427e+05       5.517e+05
v  Local Time Step            0.01        0.028531            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6046      2.3721e+06          449.68          56.562


 TIME FOR THE TIME STEP              415:        0.18175E+03

===============================================================


 INSTANT    0.416000000E+02   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        -0.114464963E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245763E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.91858E+01 0.35984E+01
   Friction velocity        uet   :  0.32104E-01 0.51795E+02
   Friction velocity        uk    :  0.32385E-01 0.51795E+02
   Dimensionless distance   yplus :  0.40374E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8469
   Nb of faces within the viscous sub-layer     :      16432
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23723E+01     554   0.22128E+00   0.23335E+01 0.29783E+01 
c  Velocity[X]                                      0.60941E+00 
c  Velocity[Y]                                      0.94310E+00 
c  Velocity[Z]                                      0.78096E+00 
c  Pressure     0.14998E+00    1289   0.39132E-01   0.66615E-01 0.67746E+00 
c  k            0.16332E+00     141   0.10459E-03   0.26022E-03 0.17894E+01 
c  epsilon      0.12141E+04      94   0.59795E-03   0.21077E+06 0.17192E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00064333                           207
a  epsilon                 -4.5489                           204
a  Local Time Step      4.2278e-08                        281777


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.7339          9.6936          1.1001         0.25957
v  Velocity[Y]              -8.122          14.388         0.85027         0.61812
v  Velocity[Z]              -11.64          7.9856        -0.61963       -0.011444
v  ǁVelocityǁ            0.0074317          15.983          3.8692          4.9523
v  Pressure                 -10032           97367           64681           51951
v  k                    2.5332e-08           2.292        0.030773        0.045616
v  epsilon               0.0012539      2.1285e+05          434.31          25.568
v  TurbVisc             3.8133e-13         0.32658       0.0015735         0.02618
v  CourantNb               0.12186      1.6593e+05          233.52          53.642
v  FourierNb               0.22414      2.3653e+06          218.04          3.0459
v  total_pressure       4.8997e+05      5.9737e+05      5.6468e+05      5.5195e+05
v  Local Time Step            0.01        0.020301            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5052       2.368e+06          451.56          56.688


 TIME FOR THE TIME STEP              416:        0.18360E+03

===============================================================


 INSTANT    0.417000000E+02   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        -0.579294179E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245741E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.93676E+01 0.35982E+01
   Friction velocity        uet   :  0.31826E-01 0.51049E+02
   Friction velocity        uk    :  0.40794E-01 0.51049E+02
   Dimensionless distance   yplus :  0.30809E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8575
   Nb of faces within the viscous sub-layer     :      16312
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23782E+01     554   0.22241E+00   0.21134E+01 0.28293E+01 
c  Velocity[X]                                      0.55239E+00 
c  Velocity[Y]                                      0.92104E+00 
c  Velocity[Z]                                      0.64001E+00 
c  Pressure     0.14237E+00    1306   0.35768E-01   0.61742E-01 0.74464E+00 
c  k            0.16344E+00     143   0.10155E-03   0.25723E-03 0.17782E+01 
c  epsilon      0.12541E+04      99   0.75093E-03   0.20792E+06 0.16534E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.0171e-05                             1
a  epsilon                 -4.3254                             6
a  Local Time Step      4.2278e-08                        281776


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.7832          9.9281          1.1069         0.25913
v  Velocity[Y]             -8.1961          14.517         0.83854         0.61763
v  Velocity[Z]              -11.66          7.7104         -0.6323       -0.010052
v  ǁVelocityǁ            0.0088492          16.044          3.9147          4.9631
v  Pressure                -9995.1           98660           65681           52652
v  k                    5.2722e-08          2.4161        0.031406        0.045675
v  epsilon               0.0024376      2.4719e+05           454.4           25.92
v  TurbVisc             1.0717e-13         0.32658       0.0015749        0.026175
v  CourantNb              0.022352      1.6497e+05           237.8          53.901
v  FourierNb               0.22365      2.3653e+06          218.05          3.0466
v  total_pressure          4.9e+05      5.9866e+05      5.6568e+05      5.5265e+05
v  Local Time Step            0.01        0.024565            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.3732      2.3717e+06          455.85          56.948


 TIME FOR THE TIME STEP              418:        0.18236E+03

===============================================================


 INSTANT    0.419000000E+02   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        -0.215085106E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245751E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           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 : -0.93676E+01 0.35982E+01
   Friction velocity        uet   :  0.31826E-01 0.51049E+02
   Friction velocity        uk    :  0.40794E-01 0.51049E+02
   Dimensionless distance   yplus :  0.30809E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8575
   Nb of faces within the viscous sub-layer     :      16312
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23782E+01     554   0.22241E+00   0.21134E+01 0.28293E+01 
c  Velocity[X]                                      0.55239E+00 
c  Velocity[Y]                                      0.92104E+00 
c  Velocity[Z]                                      0.64001E+00 
c  Pressure     0.14237E+00    1306   0.35768E-01   0.61742E-01 0.74464E+00 
c  k            0.16344E+00     143   0.10155E-03   0.25723E-03 0.17782E+01 
c  epsilon      0.12541E+04      99   0.75093E-03   0.20792E+06 0.16534E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.0171e-05                             1
a  epsilon                 -4.3254                             6
a  Local Time Step      4.2278e-08                        281776


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.7832          9.9281          1.1069         0.25913
v  Velocity[Y]             -8.1961          14.517         0.83854         0.61763
v  Velocity[Z]              -11.66          7.7104         -0.6323       -0.010052
v  ǁVelocityǁ            0.0088492          16.044          3.9147          4.9631
v  Pressure                -9995.1           98660           65681           52652
v  k                    5.2722e-08          2.4161        0.031406        0.045675
v  epsilon               0.0024376      2.4719e+05           454.4           25.92
v  TurbVisc             1.0717e-13         0.32658       0.0015749        0.026175
v  CourantNb              0.022352      1.6497e+05           237.8          53.901
v  FourierNb               0.22365      
  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5604      2.3801e+06          457.31          57.075


 TIME FOR THE TIME STEP              419:        0.18427E+03

===============================================================


 INSTANT    0.420000000E+02   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        -0.352233244E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245765E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.93833E+01 0.35981E+01
   Friction velocity        uet   :  0.31759E-01 0.48801E+02
   Friction velocity        uk    :  0.31392E-01 0.48801E+02
   Dimensionless distance   yplus :  0.38278E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8673
   Nb of faces within the viscous sub-layer     :      16159
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23866E+01     548   0.23366E+00   0.20070E+01 0.27528E+01 
c  Velocity[X]                                      0.56293E+00 
c  Velocity[Y]                                      0.89278E+00 
c  Velocity[Z]                                      0.55127E+00 
c  Pressure     0.12783E+00    1304   0.31099E-01   0.54359E-01 0.72188E+00 
c  k            0.16355E+00     138   0.10367E-03   0.26169E-03 0.17924E+01 
c  epsilon      0.12881E+04     100   0.67132E-03   0.28782E+06 0.18780E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00010637                             7
a  epsilon                 -2.3464                            25
a  Local Time Step      4.2278e-08                        281774


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -4.799          9.9531          1.1119         0.25957
v  Velocity[Y]             -8.2252          13.637         0.84401         0.61869
v  Velocity[Z]             -11.664          8.3732        -0.63611       -0.008648
v  ǁVelocityǁ            0.0059844          15.266          3.9387          4.9714
v  Pressure                -9843.9           99980           66737           53459
v  k                    1.1861e-07          2.9209        0.032041        0.045751
v  epsilon               0.0023717      4.3326e+05          476.83          26.236
v  TurbVisc             5.2411e-13         0.32658       0.0015795        0.026174
v  CourantNb                0.0435      1.9106e+05          240.55          54.119
v  FourierNb               0.22343      2.3653e+06          218.07          3.0468
v  total_pressure       4.9016e+05      5.9998e+05      5.6674e+05      5.5346e+05
v  Local Time Step            0.01        0.022282            0.01        0.010001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  -------------
  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5604      2.3801e+06          457.31          57.075


 TIME FOR THE TIME STEP              419:        0.18739E+03

===============================================================


 INSTANT    0.420000000E+02   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        -0.352233244E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245765E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.93833E+01 0.35981E+01
   Friction velocity        uet   :  0.31759E-01 0.48801E+02
   Friction velocity        uk    :  0.31392E-01 0.48801E+02
   Dimensionless distance   yplus :  0.38278E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8673
   Nb of faces within the viscous sub-layer     :      16159
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23866E+01     548   0.23366E+00   0.20070E+01 0.27528E+01 
c  Velocity[X]                                      0.56293E+00 
c  Velocity[Y]                                      0.89278E+00 
c  Velocity[Z]                                      0.55127E+00 
c  Pressure     0.12783E+00    1304   0.31099E-01   0.54359E-01 0.72188E+00 
c  k            0.16355E+00     138   0.10367E-03   0.26169E-03 0.17924E+01 
c  epsilon      0.12881E+04     100   0.67132E-03   0.28782E+06 0.18780E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00010637                             7
a  epsilon                 -2.3464                            25
a  Local Time Step      4.2278e-08                        281774


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -4.799          9.9531          1.1119         0.25957
v  Velocity[Y]             -8.2252          13.637         0.84401         0.61869
v  Velocity[Z]             -11.664          8.3732        -0.63611       -0.008648
v  ǁVelocityǁ            0.0059844          15.266          3.9387          4.9714
v  Pressure                -9843.9           99980           66737           53459
v  k                    1.1861e-07          2.9209        0.032041        0.045751
v  epsilon               0.0023717      4.3326e+05          476.83          26.236
v  TurbVisc             5.2411e-13         0.32658       0.0015795        0.026174
v  CourantNb                0.0435      1.9106e+05          240.55          54.119
v  FourierNb               0.22343      2.3653e+06          218.07          3.0468
v  total_pressure       4.9016e+05      5.9998e+05      5.6674e+05      5.5346e+05
v  Local Time Step            0.01        0.022282            0.01        0.010001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5404      2.3857e+06          458.62          57.166


 TIME FOR THE TIME STEP              420:        0.18517E+03

===============================================================


 INSTANT    0.421000000E+02   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        -0.252526300E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245756E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.93848E+01 0.37287E+01
   Friction velocity        uet   :  0.32440E-01 0.50912E+02
   Friction velocity        uk    :  0.32545E-01 0.50912E+02
   Dimensionless distance   yplus :  0.40762E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8706
   Nb of faces within the viscous sub-layer     :      16094
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23846E+01     546   0.23191E+00   0.21375E+01 0.28388E+01 
c  Velocity[X]                                      0.66521E+00 
c  Velocity[Y]                                      0.96470E+00 
c  Velocity[Z]                                      0.50758E+00 
c  Pressure     0.12189E+00    1305   0.28949E-01   0.51400E-01 0.64651E+00 
c  k            0.16357E+00     133   0.92404E-04   0.22792E-03 0.16721E+01 
c  epsilon      0.12829E+04      92   0.50358E-03   0.15107E+06 0.13676E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.8045e-05                            11
a  epsilon                 -5.9138                            17
a  Local Time Step      4.2278e-08                        281777


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.7538          10.044          1.1207         0.25974
v  Velocity[Y]             -8.2618           12.89         0.83815         0.61941
v  Velocity[Z]             -11.713          8.4839        -0.64006      -0.0080068
v  ǁVelocityǁ            0.0076699           15.19          3.9624           4.976
v  Pressure                  -9768      1.0056e+05           67219           53833
v  k                    1.2141e-07           2.301        0.032173        0.045779
v  epsilon              0.00071871      3.1143e+05          476.08          26.298
v  TurbVisc             4.6776e-13         0.32658       0.0015839        0.026176
v  CourantNb              0.089447      2.0787e+05          240.93          54.185
v  FourierNb                0.2234      2.3653e+06          218.08          3.0464
v  total_pressure       4.9023e+05      6.0056e+05      5.6722e+05      5.5383e+05
v  Local Time Step            0.01        0.015448            0.01        0.010001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5315      2.3844e+06          459.02          57.231


 TIME FOR THE TIME STEP              421:        0.18466E+03

===============================================================


 INSTANT    0.422000000E+02   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        -0.265378073E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245752E+01
Free inlet               13           0         0.000000000E+00
Convective 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        uk    :  0.33461E-01 0.54144E+02
   Dimensionless distance   yplus :  0.48073E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8787
   Nb of faces within the viscous sub-layer     :      15968
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23882E+01     548   0.22964E+00   0.28490E+01 0.32711E+01 
c  Velocity[X]                                      0.71049E+00 
c  Velocity[Y]                                      0.15827E+01 
c  Velocity[Z]                                      0.55579E+00 
c  Pressure     0.11241E+00    1301   0.25503E-01   0.46651E-01 0.59418E+00 
c  k            0.16366E+00     135   0.10983E-03   0.23178E-03 0.16854E+01 
c  epsilon      0.13026E+04      89   0.76646E-03   0.24552E+06 0.16966E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00088618                            10
a  epsilon                 -13.658                            30
a  Local Time Step      4.1945e-08                        281779


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.8289           10.08          1.1115         0.26047
v  Velocity[Y]             -8.4561          12.445         0.86989         0.61964
v  Velocity[Z]             -11.742          8.5431        -0.65136      -0.0072046
v  ǁVelocityǁ            0.0060952          14.123          3.9935          4.9853
v  Pressure                -9719.4      1.0164e+05           68131           54546
v  k                    1.2008e-07          3.3029        0.032888        0.045878
v  epsilon               0.0036344      4.9482e+05          497.86          26.604
v  TurbVisc             4.8013e-13         0.32658       0.0015911        0.026182
v  CourantNb             0.0098929      2.3841e+05          243.95          54.393
v  FourierNb               0.22345      2.3653e+06          218.12          3.0473
v  total_pressure       4.9028e+05      6.0164e+05      5.6813e+05      5.5455e+05
v  Local Time Step            0.01        0.014446            0.01        0.010001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5611      2.3931e+06          462.06          57.441


 TIME FOR THE TIME STEP              423:        0.17629E+03

=====================   Friction velocity        uk    :  0.33461E-01 0.54144E+02
   Dimensionless distance   yplus :  0.48073E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8787
   Nb of faces within the viscous sub-layer     :      15968
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23882E+01     548   0.22964E+00   0.28490E+01 0.32711E+01 
c  Velocity[X]                                      0.71049E+00 
c  Velocity[Y]                                      0.15827E+01 
c  Velocity[Z]                                      0.55579E+00 
c  Pressure     0.11241E+00    1301   0.25503E-01   0.46651E-01 0.59418E+00 
c  k            0.16366E+00     135   0.10983E-03   0.23178E-03 0.16854E+01 
c  epsilon      0.13026E+04      89   0.76646E-03   0.24552E+06 0.16966E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00088618                            10
a  epsilon                 -13.658                            30
a  Local   Friction velocity        uk    :  0.33461E-01 0.54144E+02
   Dimensionless distance   yplus :  0.48073E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8787
   Nb of faces within the viscous sub-layer     :      15968
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23882E+01     548   0.22964E+00   0.28490E+01 0.32711E+01 
c  Velocity[X]                                      0.71049E+00 
c  Velocity[Y]                                      0.15827E+01 
c  Velocity[Z]                                      0.55579E+00 
c  Pressure     0.11241E+00    1301   0.25503E-01   0.46651E-01 0.59418E+00 
c  k            0.16366E+00     135   0.10983E-03   0.23178E-03 0.16854E+01 
c  epsilon      0.13026E+04      89   0.76646E-03   0.24552E+06 0.16966E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00088618                            10
a  epsilon                 -13.658                            30
a  Local Time Step      4.1945e-08                        281779


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.8289           10.08          1.1115         0.26047
v  Velocity[Y]             -8.4561          12.445         0.86989         0.61964
v  Velocity[Z]             -11.742          8.5431        -0.65136      -0.0072046
v  ǁVelocityǁ            0.0060952          14.123          3.9935          4.9853
v  Pressure                -9719.4      1.0164e+05           68131           54546
v  k                    1.2008e-07          3.3029        0.032888        0.045878
v  epsilon               0.0036344      4.9482e+05          497.86          26.604
v  TurbVisc             4.8013e-13         0.32658       0.0015911        0.026182
v  CourantNb             0.0098929      2.3841e+05          243.95          54.393
v  FourierNb               0.22345      2.3653e+06          218.12          3.0473
v  total_pressure       4.9028e+05      6.0164e+05      5.6813e+05      5.5455e+05
v  Local Time Step            0.01        0.014446            0.01        0.010001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  ===============================================================


 INSTANT    0.425000000E+02   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        -0.145159115E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245758E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.93598E+01 0.38011E+01
   Friction velocity        uet   :  0.26114E-01 0.53794E+02
   Friction velocity        uk    :  0.28217E-01 0.53794E+02
   Dimensionless distance   yplus :  0.33230E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8856
   Nb of faces within the viscous sub-layer     :      15881
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23967E+01     546   0.23252E+00   0.31707E+01 0.34465E+01 
c  Velocity[X]                                      0.76952E+00 
c  Velocity[Y]                                      0.17827E+01 
c  Velocity[Z]                                      0.61850E+00 
c  Pressure     0.10948E+00    1266   0.23748E-01   0.44776E-01 0.46647E+00 
c  k            0.16375E+00     135   0.12509E-03   0.30539E-03 0.19335E+01 
c  epsilon      0.13466E+04      89   0.34351E-02   0.68206E+06 0.26988E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00014358                             7
a  epsilon                -0.56513                            19
a  Local Time Step      4.1039e-08                        281781


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean  ===============================================================


 INSTANT    0.425000000E+02   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        -0.145159115E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245758E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.93598E+01 0.38011E+01
   Friction velocity        uet   :  0.26114E-01 0.53794E+02
   Friction velocity        uk    :  0.28217E-01 0.53794E+02
   Dimensionless distance   yplus :  0.33230E-02 0.16023E+02
   ------------------------------------------------------
   Nb of ===============================================================


 INSTANT    0.425000000E+02   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        -0.145159115E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245758E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.93598E+01 0.38011E+01
   Friction velocity        uet   :  0.26114E-01 0.53794E+02
   Friction velocity        uk    :  0.28217E-01 0.53794E+02
   Dimensionless distance   yplus :  0.33230E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8856
   Nb of faces within the viscous sub-layer     :      15881
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23967E+01     546   0.23252E+00   0.31707E+01 0.34465E+01 
c  Velocity[X]                                      0.76952E+00 
c  Velocity[Y]                                      0.17827E+01 
c  Velocity[Z]                                      0.61850E+00 
c  Pressure     0.10948E+00    1266   0.23748E-01   0.44776E-01 0.46647E+00 
c  k            0.16375E+00     135   0.12509E-03   0.30539E-03 0.19335E+01 
c  epsilon      0.13466E+04      89   0.34351E-02   0.68206E+06 0.26988E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00014358                             7
a  epsilon                -0.56513                            19
a  Local Time Step      4.1039e-08                        281781


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.8036          10.207          1.1291         0.26119
v  Velocity[Y]             -8.5763          12.328         0.84906         0.62166
v  Velocity[Z]             -11.551          7.5136        -0.64947      -0.0071282
v  ǁVelocityǁ            0.0075896          13.999          4.0064          4.9924
v  Pressure                -9657.6      1.0257e+05           68933           55177
v  k                     6.734e-08          3.7163        0.033459        0.045962
v  epsilon               0.0020214      6.7051e+05          514.34          26.873
v  TurbVisc             5.3088e-13         0.32658       0.0016007        0.026188
v  CourantNb              0.057362      2.4367e+05          245.36          54.525
v  FourierNb               0.22346      2.3653e+06          218.13          3.0464
v  total_pressure       4.9034e+05      6.0257e+05      5.6893e+05      5.5518e+05
v  Local Time Step            0.01        0.017192            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5601      2.3705e+06          463.49          57.571


 TIME FOR THE TIME STEP              425:        0.18721E+03

===============================================================


 INSTANT    0.426000000E+02   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        -0.150942121E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245753E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.92909E+01 0.39107E+01
   Friction velocity        uet   :  0.29648E-01 0.54998E+02
   Friction velocity        uk    :  0.28727E-01 0.54998E+02
   Dimensionless distance   yplus :  0.33450E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8877
   Nb of faces within the viscous sub-layer     :      15836
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23994E+01     542   0.23443E+00   0.28772E+01 0.32800E+01 
c  Velocity[X]                                      0.74967E+00 
c  Velocity[Y]                                      0.13498E+01 
c  Velocity[Z]                                      0.77772E+00 
c  Pressure     0.10815E+00    1261   0.22978E-01   0.43895E-01 0.41461E+00 
c  k            0.16374E+00     134   0.15562E-03   0.36483E-03 0.21128E+01 
c  epsilon      0.13205E+04      91   0.22178E-02   0.34550E+06 0.20099E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.0925e-05                             2
a  epsilon                -0.64221                             2
a  Local Time Step      3.9007e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.8198          10.208          1.1213          0.2619
v  Velocity[Y]             -8.5789          12.714         0.85241         0.62187
v  Velocity[Z]             -11.711          8.3211        -0.66549      -0.0069524
v  ǁVelocityǁ             0.007084          14.234          4.0308          4.9968
v  Pressure                -9679.5      1.0294e+05           69254           55429
v  k                    1.0397e-07          2.5678        0.033321        0.046003
v  epsilon               0.0023003      3.2968e+05          499.15           26.92
v  TurbVisc             2.4672e-13         0.32658       0.0016076        0.026191
v  CourantNb              0.041601      2.5637e+05          244.83          54.595
v  FourierNb               0.22347      2.3653e+06          218.14          3.0485
v  total_pressure       4.9032e+05      6.0294e+05      5.6925e+05      5.5543e+05
v  Local Time Step            0.01        0.018911            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5804      2.3818e+06          462.97          57.643


 TIME FOR THE TIME STEP              426:        0.18353E+03

===============================================================


 INSTANT    0.427000000E+02   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        -0.377007982E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245760E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.93142E+01 0.38618E+01
   Friction velocity        uet   :  0.19982E-01 0.55181E+02
   Friction velocity        uk    :  0.19917E-01 0.55181E+02
   Dimensionless distance   ypl   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24029E+01     550   0.23446E+00   0.30988E+01 0.33982E+01 
c  Velocity[X]                                      0.84994E+00 
c  Velocity[Y]                                      0.15382E+01 
c  Velocity[Z]                                      0.71069E+00 
c  Pressure     0.10273E+00    1189   0.20980E-01   0.41161E-01 0.26574E+00 
c  k            0.16385E+00     132   0.12110E-03   0.32989E-03 0.20078E+01 
c  epsilon      0.13553E+04      90   0.54796E-03   0.14290E+06 0.12536E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0022951                            39
a  epsilon                 -26.231                            69
a  Local Time Step      3.7656e-08                        281776


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.9856          10.234          1.1098         0.26165
v  Velocity[Y]             -8.6789          12.389         0.89398         0.62121
v  Velocity[Z]             -11.561          8.5108        -0.67431      -0.0080779
v  ǁVelocityǁ            0.0088736          14.041          4.0673          5.0041
v  Pressure                -9812.6      1.0352e+05           69710           55780
v  k                    1.1594e-07          2.6674        0.033992        0.046089
v  epsilon              0.00028843      3.5486e+05          522.05          27.158
v  TurbVisc             4.5612e-13         0.32658       0.0016109        0.026196
v  CourantNb               0.13831      2.6556e+05          248.52           54.76
v  FourierNb               0.22346      2.3653e+06          218.16          3.0484
v  total_pressure       4.9019e+05      6.0352e+05      5.6971e+05      5.5578e+05
v  Local Time Step            0.01        0.022882            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.611      2.3911e+06          466.68          57.808


 TIME FOR THE TIME STEP              428:        0.17347E+03

===============================================================


 INSTANT    0.429000000E+02   TIME STEP NUMBER             429
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24029E+01     550   0.23446E+00   0.30988E+01 0.33982E+01 
c  Velocity[X]                                      0.84994E+00 
c  Velocity[Y]                                      0.15382E+01 
c  Velocity[Z]                                      0.71069E+00 
c  Pressure     0.10273E+00    1189   0.20980E-01   0.41161E-01 0.26574E+00 
c  k            0.16385E+00     132   0.12110E-03   0.32989E-03 0.20078E+01 
c  epsilon      0.13553E+04      90   0.54796E-03   0.14290E+06 0.12536E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0022951                            39
a  epsilon                 -26.231                            69
a  Local Time Step      3.7656e-08                        281776


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]     Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24029E+01     550   0.23446E+00   0.30988E+01 0.33982E+01 
c  Velocity[X]                                      0.84994E+00 
c  Velocity[Y]                                      0.15382E+01 
c  Velocity[Z]                                      0.71069E+00 
c  Pressure     0.10273E+00    1189   0.20980E-01   0.41161E-01 0.26574E+00 
c  k            0.16385E+00     132   0.12110E-03   0.32989E-03 0.20078E+01 
c  epsilon      0.13553E+04      90   0.54796E-03   0.14290E+06 0.12536E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0022951                            39
a  epsilon                 -26.231                            69
a  Local Time Step      3.7656e-08                        281776


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.9856          10.234          1.1098         0.26165
v  Velocity[Y]             -8.6789          12.389         0.89398         0.62121
v  Velocity[Z]             -11.561          8.5108        -0.67431      -0.0080779
v  ǁVelocityǁ            0.0088736          14.041          4.0673          5.0041
v  Pressure                -9812.6      1.0352e+05           69710           55780
v  k                    1.1594e-07          2.6674        0.033992        0.046089
v  epsilon              0.00028843      3.5486e+05          522.05          27.158
v  TurbVisc             4.5612e-13         0.32658       0.0016109        0.026196
v  CourantNb               0.13831      2.6556e+05          248.52           54.76
v  FourierNb               0.22346      2.3653e+06          218.16          3.0484
v  total_pressure       4.9019e+05      6.0352e+05      5.6971e+05      5.5578e+05
v  Local Time Step            0.01        0.022882            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.611      2.3911e+06          466.68          57.808


 TIME FOR THE TIME STEP              428:        0.18119E+03

==============================================================---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.165184190E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245758E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.93971E+01 0.39318E+01
   Friction velocity        uet   :  0.32371E-01 0.54309E+02
   Friction velocity        uk    :  0.43479E-01 0.54309E+02
   Dimensionless distance   yplus :  0.25569E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8967
   Nb of faces within the viscous sub-layer     :      15714
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24054E+01     560   0.23321E+00   0.36265E+01 0.36714E+01 
c  Velocity[X]                                      0.11712E+01 
c  Velocity[Y]                                      0.16672E+01 
c  Velocity[Z]                                      0.78806E+00 
c  Pressure     0.10919E+00    1066   0.20150E-01   0.43291E-01 0.14639E+00 
c  k            0.16395E+00     133   0.13493E-03   0.72208E-03 0.29653E+01 
c  epsilon      0.13538E+04     102   0.49936E-03   0.14402E+06 0.12621E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.2695e-05                             5
a  epsilon                  -1.068                            17
a  Local Time Step      3.7579e-08                        281774


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.8892          10.294          1.1198         0.26183
v  Velocity[Y]             -8.6131          12.649         0.86015         0.62153
v  Veloc---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.165184190E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245758E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.93971E+01 0.39318E+01
   Friction velocity        uet   :  0.32371E-01 0.54309E+02
   Friction velocity        uk    :  0.43479E-01 0.54309E+02
   Dimensionless distance   yplus :  0.25569E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8967
   Nb of faces within the viscous sub-layer     :      15714
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
 ---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.165184190E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245758E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.93971E+01 0.39318E+01
   Friction velocity        uet   :  0.32371E-01 0.54309E+02
   Friction velocity        uk    :  0.43479E-01 0.54309E+02
   Dimensionless distance   yplus :  0.25569E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8967
   Nb of faces within the viscous sub-layer     :      15714
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24054E+01     560   0.23321E+00   0.36265E+01 0.36714E+01 
c  Velocity[X]                                      0.11712E+01 
c  Velocity[Y]                                      0.16672E+01 
c  Velocity[Z]                                      0.78806E+00 
c  Pressure     0.10919E+00    1066   0.20150E-01   0.43291E-01 0.14639E+00 
c  k            0.16395E+00     133   0.13493E-03   0.72208E-03 0.29653E+01 
c  epsilon      0.13538E+04     102   0.49936E-03   0.14402E+06 0.12621E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.2695e-05                             5
a  epsilon                  -1.068                            17
a  Local Time Step      3.7579e-08                        281774


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  ---v  Velocity[Z]             -12.886          7.9267        -0.69197      -0.0085102
v  ǁVelocityǁ             0.030475          14.512          4.0908          5.0139
v  Pressure                 -10311      1.0398e+05           69994           55979
v  k                    1.2323e-07          2.7094        0.034498        0.046346
v  epsilon               0.0017119      3.5885e+05          529.59          27.501
v  TurbVisc             4.1089e-13         0.32658       0.0016269        0.026223
v  CourantNb              0.030135      2.6157e+05          248.27          54.922
v  FourierNb               0.22368      2.3653e+06          218.17          3.0501
v  total_pressure       4.8969e+05      6.0398e+05      5.6999e+05      5.5598e+05
v  Local Time Step            0.01        0.030457            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.545      2.3871e+06          466.44          57.972


 TIME FOR THE TIME STEP              431:        0.16653E+03

===============================================================


 INSTANT    0.432000000E+02   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        -0.172161420E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245755E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.96106E+01 0.39478E+01
   Friction velocity        uet   :  0.32837E-01 0.53029E+02
   Friction velocity        uk    :  0.32574E-01 0.53029E+02
   Dimensionless distance   yplus :  0.45214E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9045
   Nb of faces within the viscous sub-layer     :      15671
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-------------v  Velocity[Z]             -12.886          7.9267        -0.69197      -0.0085102
v  ǁVelocityǁ             0.030475          14.512          4.0908          5.0139
v  Pressure                 -10311      1.0398e+05           69994           55979
v  k                    1.2323e-07          2.7094        0.034498        0.046346
v  epsilon               0.0017119      3.5885e+05          529.59          27.501
v  TurbVisc             4.1089e-13         0.32658       0.0016269        0.026223
v  CourantNb              0.030135      2.6157e+05          248.27          54.922
v  FourierNb               0.22368      2.3653e+06          218.17          3.0501
v  total_pressure       4.8969e+05      6.0398e+05      5.6999e+05      5.5598e+05
v  Local Time Step            0.01        0.030457            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.545      2.3871e+06          466.44          57.972


 TIME FOR THE TIME STEP              431:        0.16407E+03

===============================================================


 INSTANT    0.432000000E+02   TIME STEP NUMBER             432
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet         v  Velocity[Z]             -12.886          7.9267        -0.69197      -0.0085102
v  ǁVelocityǁ             0.030475          14.512          4.0908          5.0139
v  Pressure                 -10311      1.0398e+05           69994           55979
v  k                    1.2323e-07          2.7094        0.034498        0.046346
v  epsilon               0.0017119      3.5885e+05          529.59          27.501
v  TurbVisc             4.1089e-13         0.32658       0.0016269        0.026223
v  CourantNb              0.030135      2.6157e+05          248.27          54.922
v  FourierNb               0.22368      2.3653e+06          218.17          3.0501
v  total_pressure       4.8969e+05      6.0398e+05      5.6999e+05      5.5598e+05
v  Local Time Step            0.01        0.030457            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.545      2.3871e+06          466.44          57.972


 TIME FOR THE TIME STEP              431:        0.16798E+03

===============================================================


 INSTANT    0.432000000E+02   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        -0.172161420E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245755E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.96106E+01 0.39478E+01
   Friction velocity        uet   :  0.32837E-01 0.53029E+02
   Friction velocity        uk    :  0.32574E-01 0.53029E+02
   Dimensionless distance   yplus :  0.45214E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9045
   Nb of faces within the viscous sub-layer     :      15671
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24046E+01     544   0.23447E+00   0.39973E+01 0.38481E+01 
c  Velocity[X]                                      0.11512E+01 
c  Velocity[Y]                                      0.20547E+01 
c  Velocity[Z]                                      0.79144E+00 
c  Pressure     0.11340E+00     654   0.19874E-01   0.44379E-01 0.90120E-01 
c  k            0.16426E+00     144   0.20601E-03   0.12543E-02 0.38952E+01 
c  epsilon      0.13775E+04     101   0.90282E-03   0.52703E+06 0.23181E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0032935                            28
a  epsilon                 -32.808                            69
a  Local Time Step      3.7552e-08                        281776


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.1506          10.257          1.1117         0.26259
v  Velocity[Y]             -8.5145          12.455         0.91241         0.62049
v  Velocity[Z]             -11.638          8.3251        -0.69241      -0.0089092
v  ǁVelocityǁ             0.024334          14.191          4.1142          5.0182
v  Pressure                 -10552      1.0404e+05           70005           55973
v  k                    1.1609e-07          2.6691        0.035462        0.046475
v  epsilon               0.0005788      3.6102e+05          555.23          27.801
v  TurbVisc             4.4531e-13         0.32658       0.0016345        0.026237
v  CourantNb              0.002398       2.663e+05          251.58          54.952
v  FourierNb               0.22385      2.3653e+06          218.18          3.0506
v  total_pressure       4.8945e+05      6.0404e+05      5.7001e+05      5.5597e+05
v  Local Time Step            0.01        0.033502            0.01        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6641      2.3918e+06          469.75          58.003


 TIME FOR THE TIME STEP              432:        0.15582E+03

===============================================================


 INSTANT    0.433000000E+02   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        -0.224236730E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245748E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.97411E+01 0.39743E+01
   Friction velocity        uet   :  0.21138E-01 0.52244E+02
   Friction velocity        uk    :  0.20903E-01 0.52244E+02
   Dimensionless distance   yplus :  0.37707E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9025
   Nb of faces within the viscous sub-layer     :      15646
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24092E+01     541   0.23605E+00   0.37572E+01 0.37308E+01 
c  Velocity[X]                                      0.97316E+00 
c  Velocity[Y]                                      0.19803E+01 
c  Velocity[Z]                                      0.80371E+00 
c  Pressure     0.11711E+00     907   0.19839E-01   0.45590E-01 0.94125E-01 
c  k            0.16441E+00     136   0.18122E-03   0.14816E-02 0.42222E+01 
c  epsilon      0.14039E+04      94   0.63382E-03   0.24310E+06 0.15786E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0012629                            38
a  epsilon                 -65.357                            48
a  Local Time Step      3.7891e-08                        281777


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.9735          10.256          1.1095         0.26347
v  Velocity[Y]             -8.5412          11.978         0.89443         0.62108
v  Velocity[Z]             -12.842          7.9193        -0.68821       -0.009234
v  ǁVelocityǁ             0.022102          14.501          4.1068          5.0177
v  Pressure                 -10749      1.0411e+05           70038           55980
v  k                    1.1492e-07          2.7927        0.035041        0.046595
v  epsilon               0.0005351      3.7872e+05          546.82          27.846
v  TurbVisc             4.2609e-13         0.32658       0.0016428        0.026254
v  CourantNb              0.058174      2.6392e+05          253.78          55.033
v  FourierNb                0.2239      2.3653e+06           218.2          3.0524
v  total_pressure       4.8925e+05      6.0411e+05      5.7004e+05      5.5598e+05
v  Local Time Step            0.01        0.036852            0.01        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6668      2.3894e+06          471.98          58.085


 TIME FOR THE TIME STEP              433:        0.16450E+03

===============================================================


 INSTANT    0.434000000E+02   TIME STEP NUMBER             434
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
----------------------------------------------Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245981E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99449E+01 0.39175E+01
   Friction velocity        uet   :  0.34185E-01 0.50574E+02
   Friction velocity        uk    :  0.48837E-01 0.50574E+02
   Dimensionless distance   yplus :  0.19920E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9057
   Nb of faces within the viscous sub-layer     :      15547
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24117E+01     525   0.23872E+00   0.38017E+01 0.37502E+01 
c  Velocity[X]                                      0.93573E+00 
c  Velocity[Y]                                      0.18662E+01 
c  Velocity[Z]                                      0.99980E+00 
c  Pressure     0.11497E+00     961   0.18925E-01   0.44398E-01 0.85723E-01 
c  k            0.16426E+00     133   0.17402E-03   0.12077E-02 0.38181E+01 
c  epsilon      0.13612E+04     108   0.76178E-03   0.22549E+06 0.15576E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.0269e-05                             2
a  epsilon        
a  Local Time Step      3.8305e-08                        281774


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.9193          10.206          1.1121         0.26542
v  Velocity[Y]             -8.6236          12.086         0.90248         0.62102
v  Velocity[Z]             -12.961          8.0902        -0.69495      -0.0087223
v  ǁVelocityǁ              0.01742          14.552          4.1248          5.0215
v  Pressure                 -11076       1.042e+05           70076           55977
v  k                    1.1789e-07          2.7321        0.035218        0.046713
v  epsilon                 0.00346      3.6488e+05          540.18          27.947
v  TurbVisc      Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245981E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99449E+01 0.39175E+01
   Friction velocity        uet   :  0.34185E-01 0.50574E+02
   Friction velocity        uk    :  0.48837E-01 0.50574E+02
   Dimensionless distance   yplus :  0.19920E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9057
   Nb of faces within the viscous sub-layer     :      15547
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24117E+01     525   0.23872E+00   0.38017E+01 0.37502E+01 
c  Velocity[X]                       Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245981E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99449E+01 0.39175E+01
   Friction velocity        uet   :  0.34185E-01 0.50574E+02
   Friction velocity        uk    :  0.48837E-01 0.50574E+02
   Dimensionless distance   yplus :  0.19920E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9057
   Nb of faces within the viscous sub-layer     :      15547
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24117E+01     525   0.23872E+00   0.38017E+01 0.37502E+01 
c  Velocity[X]                                      0.93573E+00 
c  Velocity[Y]                                      0.18662E+01 
c  Velocity[Z]                                      0.99980E+00 
c  Pressure     0.11497E+00     961   0.18925E-01   0.44398E-01 0.85723E-01 
c  k            0.16426E+00     133   0.17402E-03   0.12077E-02 0.38181E+01 
c  epsilon      0.13612E+04     108   0.76178E-03   0.22549E+06 0.15576E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.0269e-05                             2
a  epsilon        
a  Local Time Step      3.8305e-08                        281774


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.9193          10.206          1.1121         0.26542
v  Velocity[Y]             -8.6236          12.086         0.90248         0.62102
v  Velocity[Z]             -12.961          8.0902        -0.69495      -0.0087223
v  ǁVelocityǁ              0.01742          14.552          4.1248          5.0215
v  Pressure                 -11076     v  TurbVisc             4.2093e-13         0.32658       0.0016633        0.026295
v  CourantNb               0.11997      2.6571e+05          253.35          55.107
v  FourierNb               0.22385      2.3653e+06          218.21          3.0552
v  total_pressure       4.8879e+05      6.0425e+05      5.7009e+05      5.5598e+05
v  Local Time Step            0.01         0.02984            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6577      2.3912e+06          471.56          58.162


 TIME FOR THE TIME STEP              436:        0.15942E+03

===============================================================


 INSTANT    0.437000000E+02   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        -0.106565916E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245747E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10137E+02 0.39821E+01
   Friction velocity        uet   :  0.21433E-01 0.50055E+02
   Friction velocity        uk    :  0.22517E-01 0.50055E+02
   Dimensionless distance   yplus :  0.26619E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9081
   Nb of faces within the viscous sub-layer     :      15543
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24126E+01     538   0.23937E+00   0.39053E+01 0.38011E+01 
c  Velocity[X]                                      0.10241E+01 
c  Velocity[Y]                                      0.19160E+01 
c  Velocity[Z]                                      0.96531E+00 
c  Pressure     0.11478E+00    1049   0.19158E-01   0.44167E-01 0.11148E+00 
c  v  TurbVisc             4.2093e-13         0.32658       0.0016633        0.026295
v  CourantNb               0.11997      2.6571e+05          253.35          55.107
v  FourierNb               0.22385      2.3653e+06          218.21          3.0552
v  total_pressure       4.8879e+05      6.0425e+05      5.7009e+05      5.5598e+05
v  Local Time Step            0.01         0.02984            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6577      2.3912e+06          471.56          58.162


 TIME FOR THE TIME STEP              436:        0.15980E+03

===============================================================


 INSTANT    0.437000000E+02   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        -0.106565916E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245747E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0        v  TurbVisc             4.2093e-13         0.32658       0.0016633        0.026295
v  CourantNb               0.11997      2.6571e+05          253.35          55.107
v  FourierNb               0.22385      2.3653e+06          218.21          3.0552
v  total_pressure       4.8879e+05      6.0425e+05      5.7009e+05      5.5598e+05
v  Local Time Step            0.01         0.02984            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6577      2.3912e+06          471.56          58.162


 TIME FOR THE TIME STEP              436:        0.15868E+03

===============================================================


 INSTANT    0.437000000E+02   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        -0.106565916E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245747E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10137E+02 0.39821E+01
   Friction velocity        uet   :  0.21433E-01 0.50055E+02
   Friction velocity        uk    :  0.22517E-01 0.50055E+02
   Dimensionless distance   yplus :  0.26619E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9081
   Nb of faces within the viscous sub-layer     :      15543
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24126E+01     538   0.23937E+00   0.39053E+01 0.38011E+01 
c  Velocity[X]                                      0.10241E+01 
c  Velocity[Y]                                      0.19160E+01 
c  Velocity[Z]                                      0.96531E+00 
c  Pressure     0.11478E+00    1049   0.19158E-01   0.44167E-01 0.11148E+00 
c  k            0.16419E+00     132   0.13897E-03   0.77088E-03 0.30598E+01 
c  epsilon      0.14210E+04      92   0.53418E-03   0.11805E+06 0.10859E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00037766                             4
a  epsilon                 -4.4208                            11
a  Local Time Step      3.7833e-08                        281774


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.0678          10.234           1.101         0.26651
v  Velocity[Y]             -8.5437          12.131         0.91028         0.62085
v  Velocity[Z]              -11.87          8.0474        -0.69821      -0.0087622
v  ǁVelocityǁ              0.02139          13.782          4.1467          5.0212
v  Pressure                 -11301      1.0436e+05           70169           56025
v  k                    1.2852e-07          2.7729        0.035666        0.046518
v  epsilon               0.0016274       3.751e+05          564.19          28.009
v  TurbVisc             4.3175e-13         0.32658       0.0016627         0.02628
v  CourantNb                0.1697      2.6432e+05          255.03           55.13
v  FourierNb               0.22389      2.3653e+06          218.21          3.0534
v  total_pressure        4.887e+05      6.0436e+05      5.7017e+05      5.5603e+05
v  Local Time Step            0.01        0.032097            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6053      2.3898e+06          473.24          58.184


 TIME FOR THE TIME STEP              437:        0.16596E+03

===============================================================


 INSTANT    0.438000000E+02   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        -0.718286225E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245748E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10187E+02 0.40251E+01
   Friction velocity        uet   :  0.16191E-01 0.47119E+02
   Friction velocity        uk    :  0.16169E-01 0.47119E+02
   Dimensionless distance   yplus :  0.30805E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9106
   Nb of faces within the viscous sub-layer     :      15479
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24121E+01     530   0.23946E+00   0.47024E+01 0.41703E+01 
c  Velocity[X]                                      0.11185E+01 
c  Velocity[Y]                                      0.26297E+01 
c  Velocity[Z]                                      0.95422E+00 
c  Pressure     0.11784E+00    1054   0.20084E-01   0.45347E-01 0.11734E+00 
c  k            0.16417E+00     129   0.17678E-03   0.84646E-03 0.32096E+01 
c  epsilon      0.14482E+04      93   0.71513E-03   0.22260E+06 0.14564E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -3.962e-06                             1
a  epsilon        
a  Local Time Step      4.0087e-08                        281775


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.0731           10.29          1.1077         0.26668
v  Velocity[Y]             -8.5724          12.645         0.89397         0.62128
v  Velocity[Z]             -12.613          8.5635        -0.69346      -0.0082927
v  ǁVelocityǁ            0.0065013           14.37          4.1252          5.0228
v  Pressure                 -11347      1.0446e+05           70252           56083
v  k                    1.2871e-07          2.7756        0.035853        0.046449
v  epsilon              0.00051409       3.777e+05          575.31          28.034
v  TurbVisc             4.5132e-13         0.32658       0.0016636        0.026264
v  CourantNb               0.14266      2.4946e+05          256.13          55.128
v  FourierNb               0.22395      2.3653e+06          218.23          3.0529
v  total_pressure       4.8865e+05      6.0446e+05      5.7025e+05      5.5608e+05
v  Local Time Step            0.01        0.025108            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6392      2.3851e+06          474.36          58.181


 TIME FOR THE TIME STEP              438:        0.16796E+03

===============================================================


 INSTANT    0.439000000E+02   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        -0.336869770E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245740E+01
Free inlet               13           0       ---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10094E+02 0.39805E+01
   Friction velocity        uet   :  0.34906E-01 0.43517E+02
   Friction velocity        uk    :  0.40349E-01 0.43517E+02
   Dimensionless distance   yplus :  0.22235E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9144
   Nb of faces within the viscous sub-layer     :      15453
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24120E+01     546   0.23595E+00   0.45980E+01 0.41220E+01 
c  Velocity[X]                                      0.98076E+00 
c  Velocity[Y]                                      0.25195E+01 
c  Velocity[Z]                                      0.10978E+01 
c  Pressure     0.11365E+00     741   0.18941E-01   0.43538E-01 0.59905E-01 
c  k            0.16410E+00     132   0.95311E-04   0.44020E-03 0.23173E+01 
c  epsilon      0.14215E+04      91   0.54317E-03   0.95498E+05 0.97600E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -2.349e-06                             1
a  epsilon                 -27.263                             5
a  Local Time Step      4.2278e-08                        281777


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.4248          10.279          1.1065         0.26636
v  Velocity[Y]              -8.607          11.863         0.92679          0.6205
v  Velocity[Z]             -12.479           8.912         -0.7075      -0.0083581
v  ǁVelocityǁ             0.015877          14.236          4.1729          5.0268
v  Pressure                 -11511      1.0461e+05           70357           56173
v  k                    1.2498e-07          2.7199        0.035799        0.046274
v  epsilon               0.0030458      3.6714e+05          564.49          27.969
v  TurbVisc             3.8645e-13         0.32658       0.0016509        0.026236
v  CourantNb               0.12453      2.3595e+05          254.01          55.238
v  FourierNb               0.22404      2.3653e+06          218.22          3.0517
v  total_pressure       4.8849e+05      6.0461e+05      5.7036e+05      5.5617e+05
v  Local Time Step     ---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10094E+02 0.39805E+01
   Friction velocity        uet   :  0.34906E-01 0.43517E+02
   Friction velocity        uk    :  0.40349E-01 0.43517E+02
   Dimensionless distance   yplus :  0.22235E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9144
   Nb of faces within the viscous sub-layer     :      15453
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24120E+01     546   0.23595E+00   0.45980E+01 0.41220E+01 
c  Velocity[X]                                      0.98076E+00 
c  Velocity[Y]                                      0.25195E+01 
c  Velocity[Z]                                      0.10978E+01 
c  Pressure     0.11365E+00     741   0.18941E-01   0.43538E-01 0.59905E-01 
c  k            0.16410E+00     132   0.95311E-04   0.44020E-03 0.23173E+01 
c  epsilon      0.14215E+04      91   0.54317E-03   0.95498E+05 0.97600E---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10094E+02 0.39805E+01
   Friction velocity        uet   :  0.34906E-01 0.43517E+02
   Friction velocity        uk    :  0.40349E-01 0.43517E+02
   Dimensionless distance   yplus :  0.22235E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9144
   Nb of faces within the viscous sub-layer     :      15453
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24120E+01     546   0.23595E+00   0.45980E+01 0.41220E+01 
c  Velocity[X]                                      0.98076E+00 
c  Velocity[Y]                                      0.25195E+01 
c  Velocity[Z]                                      0.10978E+01 
c  Pressure     0.11365E+00     741   0.18941E-01   0.43538E-01 0.59905E-01 
c  k            0.16410E+00     132   0.95311E-04   0.44020E-03 0.23173E+01 
c  epsilon      0.14215E+04      91   0.54317E-03   0.95498E+05 0.97600E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -2.349e-06                             1
a  epsilon                 -27.263                             5
a  Local Time Step      4.2278e-08                        281777


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.4248          10.279          1.1065         0.26636
v  Velocity[Y]              -8.607          11.863         0.92679          0.6205
v  Velocity[Z]             -12.479           8.912         -0.7075      -0.0083581
v  ǁVelocityǁ             0.015877          14.236          4.1729          5.0268
v  Pressure                 -11511      1.0461e+05           70357           56173
v  k                    1.2498e-07          2.7199        0.035799        0.046274
v  epsilon               0.0030458      3.6714e+05          564.49          27.969
v  TurbVisc             3.8645e-13         0.32658       0.0016509        0.026236
v  CourantNb               0.12453     v  Local Time Step            0.01        0.023603            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5448      2.3868e+06           475.4          58.322


 TIME FOR THE TIME STEP              441:        0.16507E+03

===============================================================


 INSTANT    0.442000000E+02   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        -0.239641662E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245754E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98165E+01 0.40641E+01
   Friction velocity        uet   :  0.27729E-01 0.42891E+02
   Friction velocity        uk    :  0.37448E-01 0.42891E+02
   Dimensionless distance   yplus :  0.14463E-02 0.16024E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9171
   Nb of faces within the viscous sub-layer     :      15435
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24138E+01     557   0.23915E+00   0.44922E+01 0.40740E+01 
c  Velocity[X]                                      0.10704E+01 
c  Velocity[Y]                                      0.24262E+01 
c  Velocity[Z]                                      0.99557E+00 
c  Pressure     0.10882E+00     941   0.17915E-01   0.41555E-01 0.67865E-01 
c  k            0.16418E+00     126   0.10882E-03   0.42425E-03 0.22741E+01 
c  epsilon      0.14819E+04      89   0.70420E-03   0.38910E+06 0.18883E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               inv  Local Time Step            0.01        0.023603            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5448      2.3868e+06           475.4          58.322


 TIME FOR THE TIME STEP              441:        0.16609E+03

===============================================================


 INSTANT    0.442000000E+02   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        -0.239641662E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245754E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
-----------------------------------v  Local Time Step            0.01        0.023603            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5448      2.3868e+06           475.4          58.322


 TIME FOR THE TIME STEP              441:        0.16452E+03

===============================================================


 INSTANT    0.442000000E+02   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        -0.239641662E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245754E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98165E+01 0.40641E+01
   Friction velocity        uet   :  0.27729E-01 0.42891E+02
   Friction velocity        uk    :  0.37448E-01 0.42891E+02
   Dimensionless distance   yplus :  0.14463E-02 0.16024E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9171
   Nb of faces within the viscous sub-layer     :      15435
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24138E+01     557   0.23915E+00   0.44922E+01 0.40740E+01 
c  Velocity[X]                                      0.10704E+01 
c  Velocity[Y]                                      0.24262E+01 
c  Velocity[Z]                                      0.99557E+00 
c  Pressure     0.10882E+00     941   0.17915E-01   0.41555E-01 0.67865E-01 
c  k            0.16418E+00     126   0.10882E-03   0.42425E-03 0.22741E+01 
c  epsilon      0.14819E+04      89   0.70420E-03   0.38910E+06 0.18883E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00079874                            13
a  epsilon                 -6.4128                            40
a  Local Time Step      4.1166e-08                        281780


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.3326           10.22          1.1118         0.26611
v  Velocity[Y]             -8.6189          12.837         0.89159         0.62217
v  Velocity[Z]             -12.446          7.9936        -0.69821      -0.0087108
v  ǁVelocityǁ             0.015709          14.508           4.148          5.0266
v  Pressure                 -11820      1.0472e+05           70412           56225
v  k                    1.3088e-07          3.0097         0.03625        0.046242
v  epsilon              0.00064512      4.7816e+05          586.98          28.067
v  TurbVisc             4.8598e-13         0.32658       0.0016645        0.026212
v  CourantNb               0.19603      2.4292e+05          257.77          55.272
v  FourierNb               0.22355      2.3653e+06          218.26          3.0515
v  total_pressure       4.8818e+05      6.0472e+05      5.7041e+05      5.5623e+05
v  Local Time Step            0.01        0.025963            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5486      2.3684e+06          476.03          58.324


 TIME FOR THE TIME STEP              442:        0.16435E+03

===============================================================


 INSTANT    0.443000000E+02   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        -0.343477365E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245745E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.97289E+01 0.39803E+01
   Friction velocity        uet   :  0.26181E-01 0.42068E+02
   Friction velocity        uk    :  0.25663E-01 0.42068E+02
   Dimensionless distance   yplus :  0.22286E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9152
   Nb of faces within the viscous sub-layer     :      15401
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24148E+01     518   0.24380E+00   0.37516E+01 0.37224E+01 
c  Velocity[X]                                      0.10729E+01 
c  Velocity[Y]                                      0.18125E+01 
c  Velocity[Z]                                      0.86624E+00 
c  Pressure     0.10601E+00     902   0.16866E-01   0.40411E-01 0.57306E-01 
c  k            0.16415E+00     131   0.12381E-03   0.39805E-03 0.22026E+01 
c  epsilon      0.14316E+04      90   0.75445E-03   0.35677E+06 0.18845E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.2445e-06                             2
a  epsilon                 -3.1127                             3
a  Local Time Step       4.183e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.3961          10.236          1.1204         0.26554
v  Velocity[Y]             -8.5767          12.126         0.89347         0.62266
v  Velocity[Z]             -11.433          8.3203        -0.68916      -0.0086581
v  ǁVelocityǁ              0.01767          13.934          4.1499          5.0283
v  Pressure                 -12005      1.0475e+05           70387           56226
v  k                    1.3829e-07          2.7727        0.035862        0.046264
v  epsilon               0.0081111      3.7499e+05          562.98          27.995
v  TurbVisc             4.5607e-13         0.32658       0.0016899        0.026212
v  CourantNb               0.12268      2.3906e+05          254.55          55.211
v  FourierNb               0.22336      2.3653e+06          218.28          3.0534
v  total_pressure         4.88e+05      6.0475e+05      5.7039e+05      5.5623e+05
v  Local Time Step            0.01        0.026516            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5855      2.3817e+06          472.82          58.264


 TIME FOR THE TIME STEP              443:        0.16136E+03

===============================================================


 INSTANT    0.444000000E+02   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        -0.119224351E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245956E+01
Free inlet               13           0         0.000000000E+00
Convective 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 : -0.97368E+01 0.39768E+01
   Friction velocity        uet   :  0.38050E-01 0.40769E+02
   Friction velocity        uk    :  0.53976E-01 0.40769E+02
   Dimensionless distance   yplus :  0.25728E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9175
   Nb of faces within the viscous sub-layer     :      15418
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24142E+01     523   0.24327E+00   0.38533E+01 0.37696E+01 
c  Velocity[X]                                      0.98688E+00 
c  Velocity[Y]                                      0.20979E+01 
c  Velocity[Z]                                      0.76855E+00 
c  Pressure     0.94521E-01    1013   0.14732E-01   0.35919E-01 0.84958E-01 
c  k            0.16425E+00     134   0.13696E-03   0.48994E-03 0.24417E+01 
c  epsilon      0.14221E+04      92   0.89598E-03   0.32343E+06 0.17717E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.002233                            15
a  epsilon                 -12.976                            15
a  Local Time Step       4.109e-08                        281780


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.4033           10.29          1.1102         0.26602
v  Velocity[Y]              -8.556          12.183         0.91138         0.62345
v  Velocity[Z]             -11.463          8.0719        -0.71133      -0.0085971
v  ǁVelocityǁ             0.016734           14.01          4.1848          5.0307
v  Pressure                 -12410      1.0469e+05           70261           56142
v  k                    1.4345e-07          2.7682        0.036717         0.04641
v  epsilon               0.0077875      3.7392e+05          583.75          28.223
v  TurbVisc             6.8953e-14         0.32658       0.0016886        0.026228
v  CourantNb              0.050876      2.4337e+05          256.31          55.295
v  FourierNb               0.22338      2.3653e+06          218.26          3.0531
v  total_pressure       4.8759e+05      6.0469e+05      5.7026e+05      5.5614e+05
v  Local Time Step            0.01        0.027864            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5929      2.3799e+06          474.57          58.348


 TIME FOR THE TIME STEP              445:        0.17182E+03

===============================================================


 INSTANT    0.446000000E+02   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        -0.577846618E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245960E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.97454E+01 0.40466E+01
   Friction velocity        uet   :  0.24206E-01 0.39504E+02
   Friction velocity        uk    :  0.25727E-01 0.39504E+02
   Dimensionless distance     Rel velocity at the wall uiptn : -0.97368E+01 0.39768E+01
   Friction velocity        uet   :  0.38050E-01 0.40769E+02
   Friction velocity        uk    :  0.53976E-01 0.40769E+02
   Dimensionless distance   yplus :  0.25728E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9175
   Nb of faces within the viscous sub-layer     :      15418
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24142E+01     523   0.24327E+00   0.38533E+01 0.37696E+01 
c  Velocity[X]                                      0.98688E+00 
c  Velocity[Y]                                      0.20979E+01 
c  Velocity[Z]                                      0.76855E+00 
c  Pressure     0.94521E-01    1013   0.14732E-01   0.35919E-01 0.84958E-01 
c  k            0.16425E+00     134   0.13696E-03   0.48994E-03 0.24417E+01 
c  epsilon      0.14221E+04      92   0.89598E-03   0.32343E+06 0.17717E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.002233                            15
a  epsilon                 -12.976                            15
a  Local Time Step       4.109e-08                        281780


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.4033           10.29          1.1102         0.26602
v  Velocity[Y]              -8.556          12.183         0.91138         0.62345
v  Velocity[Z]             -11.463          8.0719        -0.71133      -0.0085971
v  ǁVelocityǁ             0.016734           14.01          4.1848          5.0307
v  Pressure                 -12410      1.0469e+05           70261           56142
v  k                    1.4345e-07          2.7682        0.036717         0.04641
v  epsilon               0.0077875      3.7392e+05          583.75          28.223
v  TurbVisc             6.8953e-14         0.32658       0.0016886        0.026228
v  CourantNb              0.050876      2.4337e+05          256.31          55.295
v  FourierNb               0.22338      2.3653e+06          218.26          3.0531
v  total_pressure       4.8759e+05      6.0469e+05      5.7026e+05      5.5614e+05
v  Local Time Step            0.01        0.027864            0.01        0.010002


  ** Computed val   Courant/Fourier          1.5804      2.3701e+06          475.93          58.367


 TIME FOR THE TIME STEP              446:        0.16637E+03

===============================================================


 INSTANT    0.447000000E+02   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        -0.155884975E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245754E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98056E+01 0.40211E+01
   Friction velocity        uet   :  0.31674E-01 0.37722E+02
   Friction velocity        uk    :  0.34685E-01 0.37722E+02
   Dimensionless distance   yplus :  0.35974E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9173
   Nb of faces within the viscous sub-layer     :      15359
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24162E+01     538   0.24638E+00   0.41688E+01 0.39198E+01 
c  Velocity[X]                                      0.10070E+01 
c  Velocity[Y]                                      0.21946E+01 
c  Velocity[Z]                                      0.96719E+00 
c  Pressure     0.90640E-01    1029   0.13730E-01   0.34296E-01 0.92783E-01 
c  k            0.16428E+00     130   0.12069E-03   0.35373E-03 0.20740E+01 
c  epsilon      0.14583E+04      93   0.87455E-03   0.27416E+06 0.16010E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00014842                             4
a  epsilon                 -23.337                            15
a  Local Time Step      4.2142e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.3649          10.329          1.1175         0.26627
v  Velocity[Y]             -8.5543          12.087         0.90466         0.62423
v  Velocity[Z]             -11.497          8.3865        -0.69827      -0.0088755
v  ǁVelocityǁ             0.016645          13.998          4.1691          5.0314
v  Pressure                 -12485      1.0486e+05           70347           56231
v  k                    1.4385e-07          2.8263        0.037003        0.046508
v  epsilon               0.0026042      3.8576e+05          591.66          28.332
v  TurbVisc             5.0191e-13         0.32658       0.0017331         0.02625
v  CourantNb               0.12192      2.3729e+05          257.77          55.303
v  FourierNb               0.22398      2.3653e+06           218.3          3.0557
v  total_pressure       4.8752e+05      6.0486e+05      5.7035e+05      5.5623e+05
v  Local Time Step            0.01        0.022325            0.01        0.010001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2668      2.3705e+06          476.07          58.358


 TIME FOR THE TIME STEP              447:        0.17033E+03

===============================================================   Courant/Fourier          1.5804      2.3701e+06          475.93          58.367


 TIME FOR THE TIME STEP              446:        0.16518E+03

===============================================================


 INSTANT    0.447000000E+02   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        -0.155884975E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245754E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98056E+01 0.40211E+01
   Friction velocity        uet   :  0.31674E-01 0.37722E+02
   Friction velocity        uk    :  0.34685E-01 0.37722E+02
   Dimensionless distance   yplus :  0.35974E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9173
   Nb of faces within the viscous sub-layer     :      15359
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24162E+01     538   0.24638E+00   0.41688E+01 0.39198E+01 
c  Velocity[X]                                      0.10070E+01 
c  Velocity[Y]                                      0.21946E+01 
c  Velocity[Z]                                      0.96719E+00 
c  Pressure     0.90640E-01    1029   0.13730E-01   0.34296E-01 0.92783E-01 
c  k            0.16428E+00     130   0.12069E-03   0.35373E-03 0.20740E+01 
c  epsilon      0.14583E+04      93   0.87455E-03   0.27416E+06 0.16010E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00014842                             4
a  epsilon                 -23.337                            15
a  Local Time Step      4.2142e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.3649          10.329          1.1175         0.26627
v  Velocity[Y]             -8.5543          12.087         0.90466         0.62423
v  Velocity[Z]             -11.497          8.3865        -0.69827      -0.0088755
v  ǁVelocityǁ             0.016645          13.998          4.1691          5.0314
v  Pressure                 -12485      1.0486e+05           70347           56231
v  k                    1.4385e-07          2.8263        0.037003        0.046508
v  epsilon               0.0026042      3.8576e+05          591.66          28.332
v  TurbVisc             5.0191e-13         0.32658       0.0017331         0.02625
v  CourantNb               0.12192      2.3729e+05          257.77          55.303
v  FourierNb               0.22398      2.3653e+06           218.3          3.0557
v  total_pressure       4.8752e+05      6.0486e+05      5.7035e+05      5.5623e+05
v  Local Time Step            0.01        0.022325            0.01        0.010001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2668      2.3705e+06          476.07          58.358


 TIME FOR THE TIME STEP              447:        0.16380E+03

===============================================================


 INSTANT    0.448000000E+02   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        -0.633797381E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245737E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98729E+01 0.40010E+01
   Friction velocity        uet   :  0.35636E-01 0.39868E+02
   Friction velocity        uk    :  0.37217E-01 0.39868E+02
   Dimensionless distance   yplus :  0.41770E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9191
   Nb of faces within the viscous sub-layer     :      15359
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24159E+01     523   0.24123E+00   0.34566E+01 0.35688E+01 
c  Velocity[X]                                      0.11570E+01 
c  Velocity[Y]                                      0.13784E+01 
c  Velocity[Z]                                      0.92124E+00 
c  Pressure     0.92915E-01     849   0.13901E-01   0.35064E-01 0.38851E-01 
c  k            0.16422E+00     127   0.13848E-03   0.46924E-03 0.23893E+01 
c  epsilon      0.14190E+04      94   0.86286E-03   0.32832E+06 0.18154E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011627                            12
a  epsilon                  -5.517                             6
a  Local Time Step      3.9682e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.4959          10.303           1.124         0.26618
v  Velocity[Y]             -8.5965          11.743         0.90221         0.62448
v  Velocity[Z]             -11.513          8.0133        -0.70274      -0.0088653
v  ǁVelocityǁ             0.014894          13.779          4.1838          5.0324
v  Pressure                 -12476      1.0489e+05           70359           56242
v  k                     1.489e-07          2.7118         0.03647         0.04652
v  epsilon               0.0058722      3.6812e+05          565.76          28.288
v  TurbVisc             5.0803e-13         0.32658       0.0017471        0.026255
v  CourantNb              0.057227      2.5201e+05             255          55.307
v  FourierNb               0.22415      2.3653e+06          218.32          3.0569
v  total_pressure       4.8752e+05      6.0489e+05      5.7036e+05      5.5624e+05
v  Local Time Step            0.01        0.024557            0.01        0.010001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5903      2.3775e+06          473.32          58.364


 TIME FOR THE TIME STEP              448:        0.15753E+03

===============================================================


 INSTANT    0.449000000E+02   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        -0.214237320E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245738E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99254E+01 0.39658E+01
   Friction velocity        uet   Nb of reversal of the velocity at the wall   :       9240
   Nb of faces within the viscous sub-layer     :      15335
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24196E+01     530   0.24018E+00   0.33131E+01 0.34934E+01 
c  Velocity[X]                                      0.99482E+00 
c  Velocity[Y]                                      0.14331E+01 
c  Velocity[Z]                                      0.88522E+00 
c  Pressure     0.90791E-01    1081   0.13890E-01   0.34165E-01 0.11972E+00 
c  k            0.16427E+00     140   0.13627E-03   0.45242E-03 0.23452E+01 
c  epsilon      0.14460E+04     101   0.82032E-03   0.26185E+06 0.15739E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00059468                             6
a  epsilon                    -5.7                             6
a  Local Time Step      4.2278e-08                        281778


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.5192           10.28          1.1101         0.26679
v  Velocity[Y]             -8.6138          12.116         0.91051         0.62499
v  Velocity[Z]             -12.511          8.1932        -0.70772      -0.0087428
v  ǁVelocityǁ             0.028162          14.303          4.2038          5.0335
v  Pressure                 -12446        1.05e+05           70445           56308
v  k                    1.4278e-07          2.7588         0.03756        0.046516
v  epsilon               0.0016647      3.7816e+05          598.54          28.473
v  TurbVisc             5.7107e-13         0.32658       0.0017671         0.02626
v  CourantNb               0.15432      1.8759e+05          258.08          55.404
v  FourierNb               0.22385      2.3653e+06           218.3          3.0587
v  total_pressure       4.8755e+05        6.05e+05      5.7044e+05      5.5631e+05
v  Local Time Step            0.01        0.029714            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.453      2.3686e+06          476.39          58.463


 TIME FOR THE TIME STEP              450:        0.16694E+03

===============================================================


 INSTANT    0.451000000E+02   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        -0.180726282E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245754E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98712E+01 0.39987E+01
   Friction velocity        uet   :  0.38468E-01 0.39666E+02
   Friction velocity        uk    :  0.41663E-01 0.39666E+02
   Dimensionless distance   yplus :  0.18687E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9259
   Nb of faces within the viscous sub-layer     :      15289
   Total number of wall faces                   :      41000
---------------------------   Nb of reversal of the velocity at the wall   :       9240
   Nb of faces within the viscous sub-layer     :      15335
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24196E+01     530   0.24018E+00   0.33131E+01 0.34934E+01 
c  Velocity[X]                                      0.99482E+00 
c  Velocity[Y]                                      0.14331E+01 
c  Velocity[Z]                                      0.88522E+00 
c  Pressure     0.90791E-01    1081   0.13890E-01   0.34165E-01 0.11972E+00 
c  k            0.16427E+00     140   0.13627E-03   0.45242E-03 0.23452E+01 
c  epsilon      0.14460E+04     101   0.82032E-03   0.26185E+06 0.15739E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00059468                             6
a  epsilon                    -5.7                             6
a  Local Time Step      4.2278e-08                        281778


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.5192           10.28          1.1101         0.26679
v  Velocity[Y]             -8.6138          12.116         0.91051         0.62499
v  Velocity[Z]             -12.511          8.1932        -0.70772      -0.0087428
v  ǁVelocityǁ             0.028162          14.303          4.2038          5.0335
v  Pressure                 -12446        1.05e+05           70445           56308
v  k                    1.4278e-07          2.7588         0.03756        0.046516
v  epsilon               0.0016647      3.7816e+05          598.54          28.473
v  TurbVisc             5.7107e-13         0.32658       0.0017671         0.02626
v  CourantNb               0.15432      1.8759e+05          258.08          55.404
v  FourierNb               0.22385      2.3653e+06           218.3          3.0587
v  total_pressure       4.8755e+05        6.05e+05      5.7044e+05      5.5631e+05
v  Local Time Step            0.01        0.029714            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.453      2.3686e+06          476.39          58.463


 TIME FOR THE TIME STEP              450:      

   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.253320560E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245743E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99272E+01 0.40309E+01
   Friction velocity        uet   :  0.40919E-01 0.35099E+02
   Friction velocity        uk    :  0.40744E-01 0.35099E+02
   Dimensionless distance   yplus :  0.35152E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9235
   Nb of faces within the viscous sub-layer     :      15304
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24180E+01     537   0.24114E+00   0.30611E+01 0.33581E+01 
c  Velocity[X]                                      0.87526E+00 
c  Velocity[Y]                                      0.13698E+01 
c  Velocity[Z]                                      0.81606E+00 
c  Pressure     0.85450E-01    1009   0.12481E-01   0.32166E-01 0.77586E-01 
c  k            0.16430E+00     138   0.15961E-03   0.49263E-03 0.24455E+01 
c  epsilon      0.14445E+04     101   0.50831E-03   0.12963E+06 0.11208E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0012624                             7
a  epsilon                 -234.18                            19
a  Local Time Step      4.1638e-08                        281778


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.5666          10.216          1.1198         0.26569
v  Velocity[Y]             -8.6282           11.96         0.90222          0.6251
v  Velocity[Z]             -12.539          8.1464        -0.69751      -0.0092531
v  ǁVelocityǁ             0.027134          14.359          4.1865          5.0347
v  Pressure                 -12467      1.0506e+05           70473           56324
v  k                    1.5034e-07          2.7657        0.037422        0.046557
v  epsilon              0.00011063        3.79e+05          576.52          28.421
v  TurbVisc             5.3931e-13         0.32658       0.0018807         0.02626
v  CourantNb               0.24235      2.4017e+05          256.72          55.349
v  FourierNb               0.22359      2.3653e+06          218.44          3.0642
v  total_pressure       4.8753e+05      6.0506e+05      5.7047e+05      5.5632e+05
v  Local Time Step            0.01        0.030879            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4517      2.3848e+06          475.15          58.413


 TIME FOR THE TIME STEP              452:        0.16494E+03

===============================================================


 INSTANT    0.453000000E+02   TIME STEP NUMBER             453
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------

   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.253320560E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245743E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99272E+01 0.40309E+01
   Friction velocity        uet   :  0.40919E-01 0.35099E+02
   Friction velocity        uk    :  0.40744E-01 0.35099E+02
   Dimensionless distance   yplus :  0.35152E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9235
   Nb of faces within the viscous sub-layer     :      15304
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24180E+01     537   0.24114E+00   0.30611E+01 0.33581E+01 
c  Velocity[X]                                      0.87526E+00 
c  Velocity[Y]                                      0.13698E+01 
c  Velocity[Z]                                      0.81606E+00 
c  Pressure     0.85450E-01    1009   0.12481E-01   0.32166E-01 0.77586E-01 
c  k            0.16430E+00     138   0.15961E-03   0.49263E-03 0.24455E+01 
c  epsilon      0.14445E+04     101   0.50831E-03   0.12963E+06 0.11208E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0012624                             7
a  epsilon                 -234.18                            19
a  Local Time Step      4.1638e-08                        281778


  ** Computed fields on cells
     ------------------------

   field                   minimum     v  Velocity[Y]              -8.602          12.166         0.92031         0.62444
v  Velocity[Z]             -11.802          8.3214        -0.71158      -0.0089596
v  ǁVelocityǁ             0.017414          14.389           4.211          5.0359
v  Pressure                 -12575      1.0497e+05           70373           56256
v  k                    1.5151e-07          2.7686        0.037596        0.046606
v  epsilon              0.00079222      3.7318e+05          577.33          28.427
v  TurbVisc             5.9108e-13         0.32658        0.001835        0.026263
v  CourantNb              0.086816       1.639e+05          255.95          55.368
v  FourierNb               0.22359      2.3653e+06          218.38          3.0631
v  total_pressure       4.8742e+05      6.0497e+05      5.7037e+05      5.5626e+05
v  Local Time Step            0.01        0.019927            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.3174      2.3724e+06          474.32          58.432


 TIME FOR THE TIME STEP              453:        0.16834E+03

===============================================================


 INSTANT    0.454000000E+02   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        -0.181211841E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245965E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98833E+01 0.40246E+01
   Friction velocity        uet   :  0.34917E-01 0.24335E+02
   Friction velocity        uk    :  0.35071E-01 0.24335E+02
   Dimensionless distance   yplus :  0.31052E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9230
   Nb of faces within the viscous sub-layer     :      15311
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variav  Velocity[Y]              -8.602          12.166         0.92031         0.62444
v  Velocity[Z]             -11.802          8.3214        -0.71158      -0.0089596
v  ǁVelocityǁ             0.017414          14.389           4.211          5.0359
v  Pressure                 -12575      1.0497e+05           70373           56256
v  k                    1.5151e-07          2.7686        0.037596        0.046606
v  epsilon              0.00079222      3.7318e+05          577.33          28.427
v  TurbVisc             5.9108e-13         0.32658        0.001835        0.026263
v  CourantNb              0.086816       1.639e+05          255.95          55.368
v  FourierNb               0.22359      2.3653e+06          218.38          3.0631
v  total_pressure       4.8742e+05      6.0497e+05      5.7037e+05      5.5626e+05
v  Local Time Step            0.01        0.019927            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.3174      2.3724e+06          474.32          58.432


 TIME FOR THE TIME STEP              453:        0.17230E+03

===============================================================


 INSTANT    0.454000000E+02   TIME STEP NUMBER             454
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass v  Velocity[Y]              -8.602          12.166         0.92031         0.62444
v  Velocity[Z]             -11.802          8.3214        -0.71158      -0.0089596
v  ǁVelocityǁ             0.017414          14.389           4.211          5.0359
v  Pressure                 -12575      1.0497e+05           70373           56256
v  k                    1.5151e-07          2.7686        0.037596        0.046606
v  epsilon              0.00079222      3.7318e+05          577.33          28.427
v  TurbVisc             5.9108e-13         0.32658        0.001835        0.026263
v  CourantNb              0.086816       1.639e+05          255.95          55.368
v  FourierNb               0.22359      2.3653e+06          218.38          3.0631
v  total_pressure       4.8742e+05      6.0497e+05      5.7037e+05      5.5626e+05
v  Local Time Step            0.01        0.019927            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.3174      2.3724e+06          474.32          58.432


 TIME FOR THE TIME STEP              453:        0.16747E+03

===============================================================


 INSTANT    0.454000000E+02   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        -0.181211841E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245965E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98833E+01 0.40246E+01
   Friction velocity        uet   :  0.34917E-01 0.24335E+02
   Friction velocity        uk    :  0.35071E-01 0.24335E+02
   Dimensionless distance   yplus :  0.31052E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9230
   Nb of faces within the viscous sub-layer     :      15311
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24224E+01     551   0.24830E+00   0.35455E+01 0.36124E+01 
c  Velocity[X]                                      0.11900E+01 
c  Velocity[Y]                                      0.16150E+01 
c  Velocity[Z]                                      0.74040E+00 
c  Pressure     0.87012E-01    1085   0.12815E-01   0.32755E-01 0.11349E+00 
c  k            0.16442E+00     140   0.17734E-03   0.68824E-03 0.28867E+01 
c  epsilon      0.14504E+04      94   0.80448E-03   0.29166E+06 0.16540E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00028122                            15
a  epsilon                 -6.8798                            22
a  Local Time Step      4.2278e-08                        281775


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.5813          10.229          1.1112         0.26481
v  Velocity[Y]             -8.5588          12.472         0.92465         0.62418
v  Velocity[Z]             -12.261          8.3789        -0.72311       -0.008862
v  ǁVelocityǁ            0.0097792          14.382          4.2099          5.0362
v  Pressure                 -12701      1.0488e+05           70272           56188
v  k                    4.3802e-09          2.7625        0.038345        0.046692
v  epsilon              0.00026378      3.7903e+05          601.21          28.676
v  TurbVisc             6.5004e-13         0.32658       0.0018442        0.026272
v  CourantNb              0.058532      2.0124e+05          258.91          55.396
v  FourierNb               0.22367      2.3653e+06          218.37           3.063
v  total_pressure        4.873e+05      6.0488e+05      5.7027e+05      5.5619e+05
v  Local Time Step            0.01        0.018513            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.1089      2.3679e+06          477.28          58.459


 TIME FOR THE TIME STEP              454:        0.17026E+03

===============================================================


 INSTANT    0.455000000E+02   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        -0.187650619E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245965E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98686E+01 0.39896E+01
   Friction velocity        uet   :  0.17476E-01 0.46313E+02
   Friction velocity        uk    :  0.17312E-01 0.46313E+02
   Dimensionless distance   yplus :  0.51127E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9251
   Nb of faces within the viscous sub-layer     :      15303
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24194E+01     547   0.24453E+00   0.34997E+01 0.35893E+01 
c  Velocity[X]                                      0.10704E+01 
c  Velocity[Y]                                      0.15395E+01 
c  Velocity[Z]                                      0.88981E+00 
c  Pressure     0.90973E-01    1015   0.13362E-01   0.34231E-01 0.88181E-01 
c  k            0.16445E+00     138   0.17994E-03   0.72886E-03 0.29684E+01 
c  epsilon      0.14651E+04      94   0.80216E-03   0.29275E+06 0.16480E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0005002                             4
a  epsilon                 -22.596                            21
a  Local Time Step      3.2839e-08                        281771


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.4291           10.38          1.1137         0.26476
v  Velocity[Y]             -8.5734          12.002         0.91181         0.62433
v  Velocity[Z]             -11.879          8.4542        -0.71512      -0.0085571
v  ǁVelocityǁ            0.0075756          14.678          4.2022          5.0339
v  Pressure                 -12780      1.0484e+05           70212           56140
v  k                    2.9922e-08          2.7978        0.038498        0.046776
v  epsilon              2.2504e-05      3.8004e+05          596.58          28.647
v  TurbVisc             7.3757e-14         0.32658       0.0018884        0.026283
v  CourantNb             0.0052905      3.0451e+05          259.81          55.404
v  FourierNb               0.22394      2.3653e+06          218.42          3.0656
v  total_pressure       4.8722e+05      6.0484e+05      5.7021e+05      5.5614e+05
v  Local Time Step            0.01        0.020364            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0895        2.43e+06          478.23          58.469


 TIME FOR THE TIME STEP              455:        0.16767E+03

===============================================================


 INSTANT    0.456000000E+02   TIME STEP NUMBER             456
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

------------------------------------------Smooth wall               5       41000        -0.264179993E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245973E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99843E+01 0.39674E+01
   Friction velocity        uet   :  0.23035E-01 0.34049E+02
   Friction velocity        uk    :  0.22876E-01 0.34049E+02
   Dimensionless distance   yplus :  0.28906E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9245
   Nb of faces within the viscous sub-layer     :      15293
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24203E+01     545   0.24153E+00   0.35515E+01 0.36141E+01 
c  Velocity[X]                                      0.11312E+01 
c  Velocity[Y]                                      0.14472E+01 
c  Velocity[Z]                                      0.97310E+00 
c  Pressure     0.91276E-01     933   0.12769E-01   0.34291E-01 0.40193E-01 
c  k            0.16439E+00     169   0.21519E-03   0.74600E-03 0.30020E+01 
c  epsilon      0.14287E+04      95   0.90964E-03   0.34849E+06 0.18533E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0050764                             5
a  epsilon                 -56.194                             6
a  Local Time Step      4.2278e-08                        281773


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.3986          10.392           1.126         0.26497
v  Velocity[Y]             -8.5542          11.955         0.90768         0.62399
v  Velocity[Z]             -11.575          8.6678         -0.7148      -0.0080711
v  ǁVelocityǁ             0.014378            14.4          4.2101          5.0363
v  Pressure                 -12738      1.0476e+05           70121           56095
v  k     Smooth wall               5       41000        -0.264179993E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245973E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99843E+01 0.39674E+01
   Friction velocity        uet   :  0.23035E-01 0.34049E+02
   Friction velocity        uk    :  0.22876E-01 0.34049E+02
   Dimensionless distance   yplus :  0.28906E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9245
   Nb of faces within the viscous sub-layer     :      15293
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
----------------------------------------------------------------Smooth wall               5       41000        -0.264179993E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245973E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99843E+01 0.39674E+01
   Friction velocity        uet   :  0.23035E-01 0.34049E+02
   Friction velocity        uk    :  0.22876E-01 0.34049E+02
   Dimensionless distance   yplus :  0.28906E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9245
   Nb of faces within the viscous sub-layer     :      15293
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24203E+01     545   0.24153E+00   0.35515E+01 0.36141E+01 
c  Velocity[X]                                      0.11312E+01 
c  Velocity[Y]                                      0.14472E+01 
c  Velocity[Z]                                      0.97310E+00 
c  Pressure     0.91276E-01     933   0.12769E-01   0.34291E-01 0.40193E-01 
c  k            0.16439E+00     169   0.21519E-03   0.74600E-03 0.30020E+01 
c  epsilon      0.14287E+04      95   0.90964E-03   0.34849E+06 0.18533E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0050764                             5
a  epsilon                 -56.194                             6
a  Local Time Step      4.2278e-08                        281773


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.3986          10.392           1.126         0.26497
v  Velocity[Y]             -8.5542          11.955         0.90768         0.62399
v  Velocity[Z]             -11.575       v  k                    1.0525e-07          2.7585        0.038691        0.046899
v  epsilon               0.0007196      3.7841e+05          582.99          28.814
v  TurbVisc             6.9557e-13         0.32658       0.0019433        0.026313
v  CourantNb               0.17469      2.6289e+05          259.07          55.431
v  FourierNb               0.22451      2.3653e+06          218.47          3.0699
v  total_pressure       4.8731e+05      6.0473e+05      5.7009e+05      5.5608e+05
v  Local Time Step            0.01        0.027104            0.01        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2111      2.3884e+06          477.54          58.501


 TIME FOR THE TIME STEP              458:        0.16601E+03

===============================================================


 INSTANT    0.459000000E+02   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        -0.765496266E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245956E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99987E+01 0.39940E+01
   Friction velocity        uet   :  0.34543E-01 0.48713E+02
   Friction velocity        uk    :  0.34186E-01 0.48713E+02
   Dimensionless distance   yplus :  0.40916E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9286
   Nb of faces within the viscous sub-layer     :      15303
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24206E+01     567   0.24145E+00   0.40362E+01 0.38525E+01 
c  Velocity[X]                                      0.12227E+01 
c  Velocity[Y]                              v  k                    1.0525e-07          2.7585        0.038691        0.046899
v  epsilon               0.0007196      3.7841e+05          582.99          28.814
v  TurbVisc             6.9557e-13         0.32658       0.0019433        0.026313
v  CourantNb               0.17469      2.6289e+05          259.07          55.431
v  FourierNb               0.22451      2.3653e+06          218.47          3.0699
v  total_pressure       4.8731e+05      6.0473e+05      5.7009e+05      5.5608e+05
v  Local Time Step            0.01        0.027104            0.01        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2111      2.3884e+06          477.54          58.501


 TIME FOR THE TIME STEP              458:        0.16482E+03

===============================================================


 INSTANT    0.459000000E+02   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        -0.765496266E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlv  k                    1.0525e-07          2.7585        0.038691        0.046899
v  epsilon               0.0007196      3.7841e+05          582.99          28.814
v  TurbVisc             6.9557e-13         0.32658       0.0019433        0.026313
v  CourantNb               0.17469      2.6289e+05          259.07          55.431
v  FourierNb               0.22451      2.3653e+06          218.47          3.0699
v  total_pressure       4.8731e+05      6.0473e+05      5.7009e+05      5.5608e+05
v  Local Time Step            0.01        0.027104            0.01        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2111      2.3884e+06          477.54          58.501


 TIME FOR THE TIME STEP              458:        0.15766E+03

===============================================================


 INSTANT    0.459000000E+02   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        -0.765496266E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245956E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99987E+01 0.39940E+01
   Friction velocity        uet   :  0.34543E-01 0.48713E+02
   Friction velocity        uk    :  0.34186E-01 0.48713E+02
   Dimensionless distance   yplus :  0.40916E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9286
   Nb of faces within the viscous sub-layer     :      15303
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24206E+01     567   0.24145E+00   0.40362E+01 0.38525E+01 
c  Velocity[X]                                      0.12227E+01 
c  Velocity[Y]                                      0.17408E+01 
c  Velocity[Z]                                      0.10728E+01 
c  Pressure     0.93713E-01     703   0.13167E-01   0.35164E-01 0.31972E-01 
c  k            0.16441E+00     146   0.20208E-03   0.71033E-03 0.29279E+01 
c  epsilon      0.14505E+04      97   0.46489E-03   0.99004E+05 0.97676E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001498                            37
a  epsilon                 -11.222                            39
a  Local Time Step      3.3031e-08                        281771


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.4603          10.328          1.1279         0.26469
v  Velocity[Y]             -8.5806           12.46         0.89392         0.62434
v  Velocity[Z]             -11.721          8.2624        -0.69983      -0.0080305
v  ǁVelocityǁ             0.019938          14.376          4.2088          5.0361
v  Pressure                 -12650      1.0473e+05           70087           56073
v  k                    6.4114e-08          2.8083        0.038539        0.046892
v  epsilon              7.2824e-05      3.8223e+05          581.23          28.794
v  TurbVisc             6.2819e-13         0.32658       0.0019555        0.026316
v  CourantNb               0.13597      3.0275e+05           259.8           55.43
v  FourierNb                0.2244      2.3653e+06          218.44          3.0704
v  total_pressure       4.8735e+05      6.0473e+05      5.7009e+05      5.5607e+05
v  Local Time Step            0.01        0.029815            0.01        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4358      2.4283e+06          478.23            58.5


 TIME FOR THE TIME STEP              459:        0.15901E+03

===============================================================


 INSTANT    0.460000000E+02   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         0.346400088E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245956E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           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 0.40425E+01
   Friction velocity        uet   :  0.23715E-01 0.48634E+02
   Friction velocity        uk    :  0.23333E-01 0.48634E+02
   Dimensionless distance   yplus :  0.45544E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9277
   Nb of faces within the viscous sub-layer     :      15336
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24200E+01     523   0.24225E+00   0.41391E+01 0.39011E+01 
c  Velocity[X]                                      0.11157E+01 
c  Velocity[Y]                                      0.21050E+01 
c  Velocity[Z]                                      0.91845E+00 
c  Pressure     0.99011E-01     736   0.14017E-01   0.37181E-01 0.35638E-01 
c  k            0.16443E+00     143   0.27501E-03   0.11354E-02 0.36964E+01 
c  epsilon      0.14611E+04      95   0.71497E-03   0.22372E+06 0.14494E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00069603                            20
a  epsilon                 -67.953                            53
a  Local Time Step      4.2278e-08                        281771


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.5725          10.327          1.1288         0.26507
v  Velocity[Y]             -8.5908          12.407         0.88173          0.6246
v  Velocity[Z]             -12.529          7.9533        -0.70157      -0.0080636
v  ǁVelocityǁ             0.013248          14.256          4.1981          5.0366
v  Pressure                 -12584      1.0475e+05           70087           56081
v  k                    4.4976e-08          2.7863        0.039061        0.046929
v  epsilon               0.0017813      3.8165e+05          593.12          28.782
v  TurbVisc             5.0052e-13         0.32658       0.0019879        0.026313
v  CourantNb               0.40979      1.7322e+05          257.96          55.416
v  FourierNb               0.22426      2.3653e+06          218.47          3.0717
v  total_pressure       4.8742e+05      6.0475e+05      5.7009e+05      5.5608e+05
v  Local Time Step            0.01        0.032796            0.01        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4416      2.3785e+06          476.43          58.488


 TIME FOR THE TIME STEP              460:        0.15600E+03

===============================================================


 INSTANT    0.461000000E+02   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        -0.147195468E-16
Rough wall                6           0       Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99841E+01 0.40003E+01
   Friction velocity        uet   :  0.27917E-01 0.42833E+02
   Friction velocity        uk    :  0.27883E-01 0.42833E+02
   Dimensionless distance   yplus :  0.40906E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9274
   Nb of faces within the viscous sub-layer     :      15262
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24197E+01     596   0.24556E+00   0.45068E+01 0.40711E+01 
c  Velocity[X]                                      0.11970E+01 
c  Velocity[Y]                                      0.21907E+01 
c  Velocity[Z]                                      0.11190E+01 
c  Pressure     0.95731E-01     833   0.14035E-01   0.35990E-01 0.34658E-01 
c  k            0.16452E+00     143   0.21896E-03   0.83776E-03 0.31732E+01 
c  epsilon      0.14205E+04     100   0.58664E-03   0.17283E+06 0.13122E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0021272                            64
a  epsilon                  -32.77                           140
a  Local Time Step      3.2392e-08                        281767


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.5616          10.257          1.1359         0.26349
v  Velocity[Y]             -8.5804          12.213         0.89548         0.62391
v  Velocity[Z]             -11.717           8.053        -0.70282      -0.0080139
v  ǁVelocityǁ             0.014267          14.342          4.1944          5.0375
v  Pressure                 -12532      1.0472e+05           70048           56070
v  k                    2.2568e-08          2.7493        0.038422        0.047009
v  epsilon              1.5825e-05      3.7049e+05          569.86          28.843
v  TurbVisc             6.3197e-13         0.32658        0.001994        0.026323
v  CourantNb               0.13126      3.0872e+05          256.53          55.4Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99841E+01 0.40003E+01
   Friction velocity        uet   :  0.27917E-01 0.42833E+02
   Friction velocity        uk    :  0.27883E-01 0.42833E+02
   Dimensionless distance   yplus :  0.40906E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9274
   Nb of faces within the viscous sub-layer     :      15262
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24197E+01     596   0.24556E+00   0.45068E+01 0.40711E+01 
c  Velocity[X]                                      0.11970E+01 
c  Velocity[Y]                                      0.21907E+01 
c  Velocity[Z]                                      0.11190E+01 
c  Pressure     0.95731E-01     83Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99841E+01 0.40003E+01
   Friction velocity        uet   :  0.27917E-01 0.42833E+02
   Friction velocity        uk    :  0.27883E-01 0.42833E+02
   Dimensionless distance   yplus :  0.40906E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9274
   Nb of faces within the viscous sub-layer     :      15262
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24197E+01     596   0.24556E+00   0.45068E+01 0.40711E+01 
c  Velocity[X]                                      0.11970E+01 
c  Velocity[Y]                                      0.21907E+01 
c  Velocity[Z]                                      0.11190E+01 
c  Pressure     0.95731E-01     833   0.14035E-01   0.35990E-01 0.34658E-01 
c  k            0.16452E+00     143   0.21896E-03   0.83776E-03 0.31732E+01 
c  epsilon      0.14205E+04     100   0.58664E-03   0.17283E+06 0.13122E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0021272                            64
a  epsilon                  -32.77                           140
a  Local Time Step      3.2392e-08                        281767


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.5616          10.257          1.1359         0.26349
v  Velocity[Y]             -8.5804          12.213         0.89548         0.62391
v  Velocity[Z]             -11.717           8.053        -0.70282      -0.0080139
v  ǁVelocityǁ             0.014267          14.342          4.1944          5.0375
v  Pressure                 -12532      1.0472e+05           70048           56070
v  k                    2.2568e-08     v  CourantNb             0.0098188        2.49e+05          256.74          55.455
v  FourierNb               0.22445      2.3653e+06          218.41          3.0729
v  total_pressure       4.8745e+05      6.0471e+05      5.7002e+05      5.5606e+05
v  Local Time Step            0.01        0.035551        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6622      2.3858e+06          475.15          58.528


 TIME FOR THE TIME STEP              463:        0.16765E+03

===============================================================


 INSTANT    0.464000000E+02   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        -0.134724040E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245982E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Uv  CourantNb             0.0098188        2.49e+05          256.74          55.455
v  FourierNb               0.22445      2.3653e+06          218.41          3.0729
v  total_pressure       4.8745e+05      6.0471e+05      5.7002e+05      5.5606e+05
v  Local Time Step            0.01        0.035551        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6622      2.3858e+06          475.15          58.528


 TIME FOR THE TIME STEP              463:        0.17223E+03

===============================================================


 INSTANT    0.464000000E+02   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        -0.134724040E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245982E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Unv  CourantNb             0.0098188        2.49e+05          256.74          55.455
v  FourierNb               0.22445      2.3653e+06          218.41          3.0729
v  total_pressure       4.8745e+05      6.0471e+05      5.7002e+05      5.5606e+05
v  Local Time Step            0.01        0.035551        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6622      2.3858e+06          475.15          58.528


 TIME FOR THE TIME STEP              463:        0.16693E+03

===============================================================


 INSTANT    0.464000000E+02   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        -0.134724040E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245982E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Unv  CourantNb             0.0098188        2.49e+05          256.74          55.455
v  FourierNb               0.22445      2.3653e+06          218.41          3.0729
v  total_pressure       4.8745e+05      6.0471e+05      5.7002e+05      5.5606e+05
v  Local Time Step            0.01        0.035551        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6622      2.3858e+06          475.15          58.528


 TIME FOR THE TIME STEP              463:        0.17135E+03

===============================================================


 INSTANT    0.464000000E+02   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        -0.134724040E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245982E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.97801E+01 0.40290E+01
   Friction velocity        uet   :  0.34549E-01 0.59447E+02
   Friction velocity        uk    :  0.36146E-01 0.59447E+02
   Dimensionless distance   yplus :  0.49332E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9236
   Nb of faces within the viscous sub-layer     :      15391
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24200E+01     559   0.24622E+00   0.42222E+01 0.39401E+01 
c  Velocity[X]                                      0.11300E+01 
c  Velocity[Y]                                      0.21562E+01 
c  Velocity[Z]                                      0.93612E+00 
c  Pressure     0.94443E-01     959   0.14052E-01   0.35591E-01 0.50976E-01 
c  k            0.16468E+00     147   0.33513E-03   0.14298E-02 0.41410E+01 
c  epsilon      0.14542E+04      93   0.77904E-03   0.30049E+06 0.16819E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0021292                            57
a  epsilon                 -24.829                            88
a  Local Time Step      4.2278e-08                        281768


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.5185          10.235          1.1238         0.26223
v  Velocity[Y]               -8.62          12.367          0.8879         0.62313
v  Velocity[Z]             -13.138          7.4233        -0.71044       -0.008656
v  ǁVelocityǁ             0.015125          14.878          4.1966          5.0378
v  Pressure                 -12568      1.0469e+05           69981           56041
v  k                    2.5748e-08          2.7886        0.039057        0.047103
v  epsilon               0.0019307      3.7903e+05          592.53          28.854
v  TurbVisc              6.034e-13         0.32658       0.0019796         0.02633
v  CourantNb              0.017075      1.8684e+05          256.33          55.445
v  FourierNb               0.22493      2.3653e+06          218.43          3.0723
v  total_pressure       4.8743e+05      6.0469e+05      5.6998e+05      5.5604e+05
v  Local Time Step            0.01         0.02906        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6607      2.3708e+06          474.76          58.517


 TIME FOR THE TIME STEP              464:        0.17562E+03

===============================================================


 INSTANT    0.465000000E+02   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        -0.182154798E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245961E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98590E+01 0.39881E+01
   Friction velocity        uet   :  0.38554E-01 0.32757E+02
   Friction velocity        uk    :  0.43860E-01 0.32757E+02
   Dimensionless distance   yplus :  0.41798E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9256
   Nb of faces within the viscous sub-layer     :      15250
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24215E+01     570   0.24855E+00   0.40138E+01 0.38416E+01 
c  Velocity[X]                                      0.12322E+01 
c  Velocity[Y]                                      0.18037E+01 
c  Velocity[Z]                                      0.97792E+00 
c  Pressure     0.91038E-01    1042   0.13180E-01   0.34304E-01 0.72952E-01 
c  k            0.16464E+00     162   0.36385E-03   0.14414E-02 0.41647E+01 
c  epsilon      0.14339E+04     130   0.60532E-03   0.26310E+06 0.16053E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0011703                            14
a  epsilon                 -6.1011                            13
a  Local Time Step      4.2278e-08                        281767


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.5004          10.304          1.1401         0.26136
v  Velocity[Y]             -8.5809          11.964         0.89382         0.62313
v  Velocity[Z]              -11.88          7.6686         -0.7095      -0.0083958
v  ǁVelocityǁ             0.016075          14.756          4.1915          5.0384
v  Pressure                 -12578      1.0463e+05           69914           56002
v  k                    7.8236e-08          2.8044        0.038816        0.047119
v  epsilon               0.0019076      3.7965e+05          577.35          29.012
v  TurbVisc             5.1523e-14         0.32658       0.0021415        0.026351
v  CourantNb            0.00047679      2.2773e+05          256.37          55.431
v  FourierNb               0.22545      2.3653e+06          218.63          3.0791
v  total_pressure       4.8742e+05      6.0463e+05      5.6991e+05        5.56e+05
v  Local Time Step            0.01        0.031966        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6457       2.368e+06             475           58.51


 TIME FOR THE TIME STEP              465:        0.17597E+03

===============================================================


 INSTANT    0.466000000E+02   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         0.127422673E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245957E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.97328E+01 0.39774E+01
   Friction velocity        uet   :  0.30772E-01 0.43909E+02
   Friction velocity        uk    :  0.30539E-01 0.43909E+02
   Dimensionless distance   yplus :  0.47570E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9307
   Nb of faces within the viscous sub-layer     :      15449
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24235E+01     556   0.24624E+00   0.46769E+01 0.41456E+01 
c  Velocity[X]                                      0.12897E+01 
c  Velocity[Y]                                      0.23057E+01 
c  Velocity[Z]                                      0.10815E+01 
c  Pressure     0.80629E-01     970   0.11268E-01   0.30340E-01 0.64056E-01 
c  k            0.16457E+00     145   0.18201E-03   0.75231E-03 0.30101E+01 
c  epsilon      0.14375E+04     114   0.66654E-03   0.23252E+06 0.15007E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00072847                            47
a  epsilon                 -9.1668                           124
a  Local Time Step      4.2278e-08                        281769


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.5745          10.286          1.1308          0.2624
v  Velocity[Y]               -8.62          12.775         0.89346         0.62382
v  Velocity[Z]              -11.81          7.8135        -0.70375      -0.0082474
v  ǁVelocityǁ            0.0096182          14.521           4.213          5.0387
v  Pressure                 -12447      1.0466e+05           69927           56017
v  k                    1.3508e-08          2.7855        0.038309        0.047078
v  epsilon              2.8666e-05      3.7692e+05          578.11          28.899
v  TurbVisc             6.1305e-13         0.32658       0.0019526        0.026345
v  CourantNb               0.22299      1.8615e+05          255.67          55.492
v  FourierNb               0.22562      2.3653e+06          218.42          3.0721
v  total_pressure       4.8755e+05      6.0466e+05      5.6993e+05      5.5602e+05
v  Local Time Step            0.01        0.038679        0.010001        0.010006


  ** Computed values on cells
     ------------   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.97328E+01 0.39774E+01
   Friction velocity        uet   :  0.30772E-01 0.43909E+02
   Friction velocity        uk    :  0.30539E-01 0.43909E+02
   Dimensionless distance   yplus :  0.47570E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9307
   Nb of faces within the viscous sub-layer     :      15449
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24235E+01     556   0.24624E+00   0.46769E+01 0.41456E+01 
c  Velocity[X]                                      0.12897E+01 
c  Velocity[Y]                                      0.23057E+01 
c  Velocity[Z]                                      0.10815E+01 
c  Pressure     0.80629E-01     970   0.11268E-01   0.30340E-01 0.64056E-01 
c  k            0.16457E+00     145   0.18201E-03   0.75231E-03 0.30101E+01 
c  epsilon      0.14375E+04     114   0.66654E-03   0.23252E+06 0.15007E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for    ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.97328E+01 0.39774E+01
   Friction velocity        uet   :  0.30772E-01 0.43909E+02
   Friction velocity        uk    :  0.30539E-01 0.43909E+02
   Dimensionless distance   yplus :  0.47570E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9307
   Nb of faces within the viscous sub-layer     :      15449
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24235E+01     556   0.24624E+00   0.46769E+01 0.41456E+01 
c  Velocity[X]                                      0.12897E+01 
c  Velocity[Y]                                      0.23057E+01 
c  Velocity[Z]                                      0.10815E+01 
c  Pressure     0.80629E-01     970   0.11268E-01   0.30340E-01 0.64056E-01 
c  k            0.16457E+00     145   0.18201E-03   0.75231E-03 0.30101E+01 
c  epsilon      0.14375E+04     114   0.66654E-03   0.23252E+06 0.15007E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00072847                            47
a  epsilon                 -9.1668                           124
a  Local Time Step      4.2278e-08                        281769


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.5745          10.286          1.1308          0.2624
v  Velocity[Y]               -8.62          12.775         0.89346         0.62382
v  Velocity[Z]              -11.81          7.8135        -0.70375      -0.0082474
v  ǁVelocityǁ            0.0096182          14.521           4.213          5.0387
v  Pressure                 -12447      1.0466e+05           69927           56017
v  k                    1.3508e-08          2.7855        0.038309        0.047078
v  epsilon              2.8666e-05      3.7692e+05          578.11          28.899
v  TurbVisc             6.1305e-13         0.32658       0.0019526        0.026345
v  CourantNb               0.22299      1.8615e+05          255.67          55.492
v  FourierNb               0.22562      
  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6354      2.3928e+06          475.96          58.561


 TIME FOR THE TIME STEP              468:        0.17455E+03

===============================================================


 INSTANT    0.469000000E+02   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         0.212450067E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245742E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.97156E+01 0.39962E+01
   Friction velocity        uet   :  0.35313E-01 0.34472E+02
   Friction velocity        uk    :  0.35312E-01 0.34472E+02
   Dimensionless distance   yplus :  0.43986E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9284
   Nb of faces within the viscous sub-layer     :      15265
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24213E+01     566   0.24696E+00   0.39913E+01 0.38307E+01 
c  Velocity[X]                                      0.12219E+01 
c  Velocity[Y]                                      0.17649E+01 
c  Velocity[Z]                                      0.10046E+01 
c  Pressure     0.85302E-01     970   0.11835E-01   0.32136E-01 0.54996E-01 
c  k            0.16459E+00     148   0.33786E-03   0.10908E-02 0.36196E+01 
c  epsilon      0.14521E+04     102   0.80982E-03   0.42839E+06 0.20143E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  ----------
  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6354      2.3928e+06          475.96          58.561


 TIME FOR THE TIME STEP              468:        0.16714E+03

===============================================================


 INSTANT    0.469000000E+02   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         0.212450067E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245742E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maxim
  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6354      2.3928e+06          475.96          58.561


 TIME FOR THE TIME STEP              468:        0.17095E+03

===============================================================


 INSTANT    0.469000000E+02   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         0.212450067E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245742E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.97156E+01 0.39962E+01
   Friction velocity        uet   :  0.35313E-01 0.34472E+02
   Friction velocity        uk    :  0.35312E-01 0.34472E+02
   Dimensionless distance   yplus :  0.43986E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9284
   Nb of faces within the viscous sub-layer     :      15265
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24213E+01     566   0.24696E+00   0.39913E+01 0.38307E+01 
c  Velocity[X]                                      0.12219E+01 
c  Velocity[Y]                                      0.17649E+01 
c  Velocity[Z]                                      0.10046E+01 
c  Pressure     0.85302E-01     970   0.11835E-01   0.32136E-01 0.54996E-01 
c  k            0.16459E+00     148   0.33786E-03   0.10908E-02 0.36196E+01 
c  epsilon      0.14521E+04     102   0.80982E-03   0.42839E+06 0.20143E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0013445                            16
a  epsilon                 -147.57                            37
a  Local Time Step      4.2278e-08                        281769


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.5044          10.226          1.1405         0.26217
v  Velocity[Y]             -8.5849          11.951         0.90952         0.62367
v  Velocity[Z]              -11.77          7.9244        -0.71275       -0.008386
v  ǁVelocityǁ             0.015345          14.438           4.203          5.0384
v  Pressure                 -12333      1.0479e+05           70019           56092
v  k                    9.5004e-08          2.8228        0.039499        0.047127
v  epsilon               0.0019792      3.8359e+05           590.9          29.099
v  TurbVisc             1.0465e-13         0.32658       0.0021103         0.02635
v  CourantNb                0.1034      2.3581e+05          258.26          55.481
v  FourierNb               0.22498      2.3653e+06          218.62          3.0795
v  total_pressure       4.8767e+05      6.0479e+05      5.7002e+05      5.5609e+05
v  Local Time Step            0.01        0.031977        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6453      2.3786e+06          476.88           58.56


 TIME FOR THE TIME STEP              469:        0.17241E+03

===============================================================


 INSTANT    0.470000000E+02   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        -0.938320529E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245755E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.96688E+01 0.40043E+01
   Friction velocity        uet   :  0.37428E-01 0.47979E+02
   Friction velocity        uk    :  0.37053E-01 0.47979E+02
   Dimensionless distance   yplus :  0.41973E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9284
   Nb of faces within the viscous sub-layer     :      15288
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24224E+01     603   0.24222E+00   0.39841E+01 0.38266E+01 
c  Velocity[X]                                      0.12098E+01 
c  Velocity[Y]                                      0.18056E+01 
c  Velocity[Z]                                      0.96870E+00 
c  Pressure     0.80343E-01     941   0.11318E-01   0.30256E-01 0.50706E-01 
c  k            0.16456E+00     141   0.25411E-03   0.77275E-03 0.30476E+01 
c  epsilon      0.14341E+04     110   0.71376E-03   0.26208E+06 0.16094E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.003746                           227
a  epsilon                 -42.642                           346
a  Local Time Step      2.9418e-08                        281771


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.6658          10.155          1.1449          0.2619
v  Velocity[Y]             -8.6568          12.204         0.89683         0.62403
v  Velocity[Z]             -12.541          8.4481        -0.70153      -0.0087303
v  ǁVelocityǁ             0.012667           14.26          4.1991           5.039
v  Pressure                 -12329      1.0483e+05           70046           56115
v  k                    1.1867e-07          2.7624        0.038833        0.047128
v  epsilon              0.00039333      3.7125e+05          572.26          28.944
v  TurbVisc             5.8932e-13         0.32658        0.002075        0.026348
v  CourantNb               0.30733      3.3993e+05          257.63          55.499
v  FourierNb               0.22487      2.3653e+06          218.54          3.0773
v  total_pressure       4.8767e+05      6.0483e+05      5.7005e+05      5.5612e+05
v  Local Time Step            0.01         0.03336        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6562      2.4654e+06          476.17          58.576


 TIME FOR THE TIME STEP              470:        0.18853E+03

===============================================================


 INSTANT    0.471000000E+02   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         0.412133318E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245748E+01
Free inlet               13           0         0.000000000E+00
Convective 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   :  0.33645E-01 0.58620E+02
   Friction velocity        uk    :  0.33643E-01 0.58620E+02
   Dimensionless distance   yplus :  0.46810E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9239
   Nb of faces within the viscous sub-layer     :      15306
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24222E+01     547   0.24572E+00   0.39147E+01 0.37929E+01 
c  Velocity[X]                                      0.10903E+01 
c  Velocity[Y]                                      0.18804E+01 
c  Velocity[Z]                                      0.94402E+00 
c  Pressure     0.85775E-01     868   0.12545E-01   0.32336E-01 0.34308E-01 
c  k            0.16456E+00     153   0.25984E-03   0.91441E-03 0.33117E+01 
c  epsilon      0.14530E+04      97   0.89071E-03   0.36119E+06 0.18401E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0013329                            39
a  epsilon                 -64.223                            38
a  Local Time Step      4.2278e-08                        281768


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.5571          10.212           1.118         0.26221
v  Velocity[Y]             -8.6372          12.605         0.92021         0.62312
v  Velocity[Z]             -12.464          7.5502        -0.72446      -0.0088214
v  ǁVelocityǁ             0.017636          14.631          4.2213          5.0386
v  Pressure                 -12488      1.0484e+05           70025           56105
v  k                    4.0346e-08          2.7705        0.039707        0.047134
v  epsilon               0.0019267        3.73e+05           602.1           28.94
v  TurbVisc             6.5837e-13         0.32658       0.0020526        0.026349
v  CourantNb               0.23955      2.0325e+05           257.2          55.461
v  FourierNb               0.22501      2.3653e+06          218.48          3.0766
v  total_pressure       4.8751e+05      6.0484e+05      5.7003e+05       5.561e+05
v  Local Time Step            0.01        0.037842        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6306      2.3972e+06          475.68          58.538


 TIME FOR THE TIME STE   Friction velocity        uet   :  0.33645E-01 0.58620E+02
   Friction velocity        uk    :  0.33643E-01 0.58620E+02
   Dimensionless distance   yplus :  0.46810E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9239
   Nb of faces within the viscous sub-layer     :      15306
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24222E+01     547   0.24572E+00   0.39147E+01 0.37929E+01 
c  Velocity[X]                                      0.10903E+01 
c  Velocity[Y]                                      0.18804E+01 
c  Velocity[Z]                                      0.94402E+00 
c  Pressure     0.85775E-01     868   0.12545E-01   0.32336E-01 0.34308E-01 
c  k            0.16456E+00     153   0.25984E-03   0.91441E-03 0.33117E+01 
c  epsilon      0.14530E+04      97   0.89071E-03   0.36119E+06 0.18401E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0013329                            39
a  epsilon     Friction velocity        uet   :  0.33645E-01 0.58620E+02
   Friction velocity        uk    :  0.33643E-01 0.58620E+02
   Dimensionless distance   yplus :  0.46810E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9239
   Nb of faces within the viscous sub-layer     :      15306
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24222E+01     547   0.24572E+00   0.39147E+01 0.37929E+01 
c  Velocity[X]                                      0.10903E+01 
c  Velocity[Y]                                      0.18804E+01 
c  Velocity[Z]                                      0.94402E+00 
c  Pressure     0.85775E-01     868   0.12545E-01   0.32336E-01 0.34308E-01 
c  k            0.16456E+00     153   0.25984E-03   0.91441E-03 0.33117E+01 
c  epsilon      0.14530E+04      97   0.89071E-03   0.36119E+06 0.18401E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0013329                            39
a  epsilon                 -64.223                            38
a  Local Time Step      4.2278e-08                        281768


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.5571          10.212           1.118         0.26221
v  Velocity[Y]             -8.6372          12.605         0.92021         0.62312
v  Velocity[Z]             -12.464          7.5502        -0.72446      -0.0088214
v  ǁVelocityǁ             0.017636          14.631          4.2213          5.0386
v  Pressure                 -12488      1.0484e+05           70025           56105
v  k                    4.0346e-08          2.7705        0.039707        0.047134
v  epsilon               0.0019267        3.73e+05           602.1           28.94
v  TurbVisc             6.5837e-13         0.32658       0.0020526        0.026349
v  CourantNb               0.23955      2.0325e+05           257.2          55.461
v  FourierNb               0.22501      2.3653e+06          218.48          3.0766
v  total_pressure       4.8751e+05      6.0484e+05      5.7003e+05       5.561e+05
v  Local Time Step            0.01        0.037842        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum        TIME FOR THE TIME STEP              473:        0.17998E+03

===============================================================


 INSTANT    0.474000000E+02   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        -0.749250879E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245967E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98406E+01 0.40146E+01
   Friction velocity        uet   :  0.30704E-01 0.44986E+02
   Friction velocity        uk    :  0.30683E-01 0.44986E+02
   Dimensionless distance   yplus :  0.40438E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9264
   Nb of faces within the viscous sub-layer     :      15327
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24195E+01     584   0.24516E+00   0.40958E+01 0.38796E+01 
c  Velocity[X]                                      0.12819E+01 
c  Velocity[Y]                                      0.18706E+01 
c  Velocity[Z]                                      0.94326E+00 
c  Pressure     0.96502E-01    1054   0.14304E-01   0.36388E-01 0.96966E-01 
c  k            0.16457E+00     169   0.37325E-03   0.99568E-03 0.34509E+01 
c  epsilon      0.14535E+04     104   0.55177E-03   0.19976E+06 0.13827E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.002125                           127
a  epsilon                 -35.304                           232
a  Local Time Step      3.0458e-08                        281770


  ** Computed fields on cells
     ------------------------

   fie TIME FOR THE TIME STEP              473:        0.18377E+03

===============================================================


 INSTANT    0.474000000E+02   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        -0.749250879E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245967E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98406E+01 0.40146E+01
   Friction velocity        uet   :  0.30704E-01 0.44986E+02
   Friction velocity        uk    :  0.30683E-01 0.44986E+02
   Dimensionless distance   yplus :  0.40438E-02 0.16023E+02
   -- TIME FOR THE TIME STEP              473:        0.18444E+03

===============================================================


 INSTANT    0.474000000E+02   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        -0.749250879E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245967E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98406E+01 0.40146E+01
   Friction velocity        uet   :  0.30704E-01 0.44986E+02
   Friction velocity        uk    :  0.30683E-01 0.44986E+02
   Dimensionless distance   yplus :  0.40438E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9264
   Nb of faces within the viscous sub-layer     :      15327
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24195E+01     584   0.24516E+00   0.40958E+01 0.38796E+01 
c  Velocity[X]                                      0.12819E+01 
c  Velocity[Y]                                      0.18706E+01 
c  Velocity[Z]                                      0.94326E+00 
c  Pressure     0.96502E-01    1054   0.14304E-01   0.36388E-01 0.96966E-01 
c  k            0.16457E+00     169   0.37325E-03   0.99568E-03 0.34509E+01 
c  epsilon      0.14535E+04     104   0.55177E-03   0.19976E+06 0.13827E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.002125                           127
a  epsilon                 -35.304                           232
a  Local Time Step      3.0458e-08                        281770


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.6441          10.268          1.1362         0.26099
v  Velocity[Y]             -8.7317          12.611         0.90601         0.62381
v  Velocity[Z]             -11.881          8.0429        -0.70747      -0.0092633
v  ǁVelocityǁ             0.010693          14.695           4.202          5.0385
v  Pressure                 -12762      1.0473e+05           69883           56002
v  k                    1.0436e-07          2.7967        0.040022        0.047225
v  epsilon              0.00040277      3.7823e+05          585.06          28.997
v  TurbVisc             8.1726e-13         0.32658       0.0022236        0.026359
v  CourantNb               0.03033      3.2832e+05          258.68          55.435
v  FourierNb               0.22527      2.3653e+06          218.72          3.0843
v  total_pressure       4.8724e+05      6.0473e+05      5.6988e+05        5.56e+05
v  Local Time Step            0.01        0.045789        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6875      2.4539e+06           477.4           58.52


 TIME FOR THE TIME STEP              474:        0.18488E+03

===============================================================


 INSTANT    0.475000000E+02   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        -0.151162761E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245970E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98104E+01 0.39604E+01
   Friction velocity        uet   :  0.38436E-01 0.43994E+02
   Friction velocity        uk    :  0.38592E-01 0.43994E+02
   Dimensionless distance   yplus :  0.33283E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9262
   Nb of faces within the viscous sub-layer     :      15352
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24188E+01     542   0.24805E+00   0.40255E+01 0.38469E+01 
c  Velocity[X]                                      0.12642E+01 
c  Velocity[Y]                                      0.17921E+01 
c  Velocity[Z]                                      0.96920E+00 
c  Pressure     0.10030E+00     904   0.14925E-01   0.37836E-01 0.45325E-01 
c  k            0.16452E+00     159   0.19007E-03   0.65908E-03 0.28085E+01 
c  epsilon      0.14512E+04      96   0.61553E-03   0.21685E+06 0.14313E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00075957                            35
a  epsilon                 -9.2996                           101
a  Local Time Step      4.2278e-08                        281768


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.4672          10.353           1.113         0.26239
v  Velocity[Y]             -8.6306          12.802         0.91182         0.62326
v  Velocity[Z]              -11.76          8.3435        -0.72079      -0.0089399
v  ǁVelocityǁ             0.010831          14.716          4.2147          5.0375
v  Pressure                 -12831      1.0472e+05           69855           55994
v  k                    1.4077e-07          2.7775        0.039981         0.04723
v  epsilon              3.3528e-05      3.7436e+05          597.66          28.967
v  TurbVisc              6.399e-13         0.32658       0.0021839        0.026364
v  CourantNb               0.24076      1.5531e+05          256.78          55.439
v  FourierNb               0.22524      2.3653e+06          218.68          3.0826
v  total_pressure       4.8717e+05      6.0472e+05      5.6986e+05      5.5599e+05
v  Local Time Step            0.01        0.050368        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6707      2.3945e+06          475.46          58.522


 TIME FOR THE TIME STEP              475:        0.16758E+03

===============================================================


 INSTANT    0.476000000E+02   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        -0.798167951E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245961E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99361E+01 0.40012E+01
   Friction velocity        uet   :  0.25999E-01 0.53597E+02
   Friction velocity        uk    :  0.25491E-01 0.53597E+02
   Dimensionless distance   ypl   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24177E+01     537   0.23688E+00   0.33840E+01 0.35271E+01 
c  Velocity[X]                                      0.11605E+01 
c  Velocity[Y]                                      0.13739E+01 
c  Velocity[Z]                                      0.84958E+00 
c  Pressure     0.93800E-01     808   0.14173E-01   0.35328E-01 0.32931E-01 
c  k            0.16450E+00     178   0.26094E-03   0.81410E-03 0.31144E+01 
c  epsilon      0.14706E+04      95   0.57374E-03   0.28906E+06 0.16401E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0013685                            71
a  epsilon                 -148.69                            92
a  Local Time Step      3.4253e-08                        281768


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.5611          10.339          1.1279         0.26232
v  Velocity[Y]             -8.6111           12.71         0.92173         0.62284
v  Velocity[Z]             -12.122          8.6129        -0.72276      -0.0090177
v  ǁVelocityǁ             0.014368          14.507          4.2187          5.0376
v  Pressure                 -12846      1.0473e+05           69848           55993
v  k                    9.3696e-08           2.801        0.041207        0.047306
v  epsilon              0.00029428      3.7974e+05          603.27          29.226
v  TurbVisc             2.3332e-14         0.32658        0.002219        0.026371
v  CourantNb               0.19757      2.9194e+05          260.45          55.492
v  FourierNb               0.22501      2.3653e+06          218.73          3.0846
v  total_pressure       4.8715e+05      6.0473e+05      5.6985e+05      5.5599e+05
v  Local Time Step            0.01        0.060945        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6689      2.4173e+06          479.19          58.577


 TIME FOR THE TIME STEP              477:        0.16394E+03

===============================================================


 INSTANT    0.478000000E+02   TIME STEP NUMBER             478
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24177E+01     537   0.23688E+00   0.33840E+01 0.35271E+01 
c  Velocity[X]                                      0.11605E+01 
c  Velocity[Y]                                      0.13739E+01 
c  Velocity[Z]                                      0.84958E+00 
c  Pressure     0.93800E-01     808   0.14173E-01   0.35328E-01 0.32931E-01 
c  k            0.16450E+00     178   0.26094E-03   0.81410E-03 0.31144E+01 
c  epsilon      0.14706E+04      95   0.57374E-03   0.28906E+06 0.16401E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0013685                            71
a  epsilon                 -148.69                            92
a  Local Time Step      3.4253e-08                        281768


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]     Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24177E+01     537   0.23688E+00   0.33840E+01 0.35271E+01 
c  Velocity[X]                                      0.11605E+01 
c  Velocity[Y]                                      0.13739E+01 
c  Velocity[Z]                                      0.84958E+00 
c  Pressure     0.93800E-01     808   0.14173E-01   0.35328E-01 0.32931E-01 
c  k            0.16450E+00     178   0.26094E-03   0.81410E-03 0.31144E+01 
c  epsilon      0.14706E+04      95   0.57374E-03   0.28906E+06 0.16401E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0013685                            71
a  epsilon                 -148.69                            92
a  Local Time Step      3.4253e-08                        281768


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.5611          10.339          1.1279         0.26232
v  Velocity[Y]             -8.6111           12.71         0.92173         0.62284
v  Velocity[Z]             -12.122          8.6129        -0.72276      -0.0090177
v  ǁVelocityǁ             0.014368          14.507          4.2187          5.0376
v  Pressure                 -12846      1.0473e+05           69848           55993
v  k                    9.3696e-08           2.801        0.041207        0.047306
v  epsilon              0.00029428      3.7974e+05          603.27          29.226
v  TurbVisc             2.3332e-14         0.32658        0.002219        0.026371
v  CourantNb               0.19757      2.9194e+05          260.45          55.492
v  FourierNb               0.22501      2.3653e+06          218.73          3.0846
v  total_pressure       4.8715e+05      6.0473e+05      5.6985e+05      5.5599e+05
v  Local Time Step            0.01        0.060945        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6689      2.4173e+06          479.19          58.577


 TIME FOR THE TIME STEP              477:        0.16578E+03

==============================================================---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.224024969E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245756E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10068E+02 0.39834E+01
   Friction velocity        uet   :  0.22613E-01 0.50895E+02
   Friction velocity        uk    :  0.22394E-01 0.50895E+02
   Dimensionless distance   yplus :  0.41518E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9262
   Nb of faces within the viscous sub-layer     :      15328
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.224024969E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245756E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10068E+02 0.39834E+01
   Friction velocity        uet   :  0.22613E-01 0.50895E+02
   Friction velocity        uk    :  0.22394E-01 0.50895E+02
   Dimensionless distance   yplus :  0.41518E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9262
   Nb of faces within the viscous sub-layer     :      15328
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
 ---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.224024969E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245756E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10068E+02 0.39834E+01
   Friction velocity        uet   :  0.22613E-01 0.50895E+02
   Friction velocity        uk    :  0.22394E-01 0.50895E+02
   Dimensionless distance   yplus :  0.41518E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9262
   Nb of faces within the viscous sub-layer     :      15328
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
 ---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.224024969E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245756E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10068E+02 0.39834E+01
   Friction velocity        uet   :  0.22613E-01 0.50895E+02
   Friction velocity        uk    :  0.22394E-01 0.50895E+02
   Dimensionless distance   yplus :  0.41518E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9262
   Nb of faces within the viscous sub-layer     :      15328
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24163E+01     552   0.24412E+00   0.34075E+01 0.35392E+01 
c  Velocity[X]                                      0.11323E+01 
c  Velocity[Y]                                      0.14167E+01 
c  Velocity[Z]                                      0.85850E+00 
c  Pressure     0.91145E-01     970   0.13560E-01   0.34310E-01 0.59233E-01 
c  k            0.16446E+00     177   0.20931E-03   0.58782E-03 0.26435E+01 
c  epsilon      0.14628E+04      97   0.71387E-03   0.24705E+06 0.15188E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0011048                            73
a  epsilon                 -12.705                           121
a  Local Time Step      4.2278e-08                        281768


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  ---v  Velocity[Z]             -11.611          7.5862        -0.72884      -0.0092174
v  ǁVelocityǁ             0.017549          14.707          4.2331          5.0383
v  Pressure                 -12615      1.0482e+05           69908           56056
v  k                    7.9842e-08          2.7805        0.041727        0.047374
v  epsilon               0.0015671      3.7548e+05           615.2          29.289
v  TurbVisc             2.5585e-14         0.32658       0.0022914        0.026375
v  CourantNb              0.068676      2.0466e+05          259.07          55.424
v  FourierNb               0.22433      2.3653e+06          218.85          3.0878
v  total_pressure       4.8739e+05      6.0482e+05      5.6991e+05      5.5606e+05
v  Local Time Step            0.01        0.034524            0.01        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6595      2.4054e+06          477.92          58.511


 TIME FOR THE TIME STEP              480:        0.16370E+03

===============================================================


 INSTANT    0.481000000E+02   TIME STEP NUMBER             481
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet        v  Velocity[Z]             -11.611          7.5862        -0.72884      -0.0092174
v  ǁVelocityǁ             0.017549          14.707          4.2331          5.0383
v  Pressure                 -12615      1.0482e+05           69908           56056
v  k                    7.9842e-08          2.7805        0.041727        0.047374
v  epsilon               0.0015671      3.7548e+05           615.2          29.289
v  TurbVisc             2.5585e-14         0.32658       0.0022914        0.026375
v  CourantNb              0.068676      2.0466e+05          259.07          55.424
v  FourierNb               0.22433      2.3653e+06          218.85          3.0878
v  total_pressure       4.8739e+05      6.0482e+05      5.6991e+05      5.5606e+05
v  Local Time Step            0.01        0.034524            0.01        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6595      2.4054e+06          477.92          58.511


 TIME FOR THE TIME STEP              480:        0.17816E+03

===============================================================


 INSTANT    0.481000000E+02   TIME STEP NUMBER             481
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet         v  Velocity[Z]             -11.611          7.5862        -0.72884      -0.0092174
v  ǁVelocityǁ             0.017549          14.707          4.2331          5.0383
v  Pressure                 -12615      1.0482e+05           69908           56056
v  k                    7.9842e-08          2.7805        0.041727        0.047374
v  epsilon               0.0015671      3.7548e+05           615.2          29.289
v  TurbVisc             2.5585e-14         0.32658       0.0022914        0.026375
v  CourantNb              0.068676      2.0466e+05          259.07          55.424
v  FourierNb               0.22433      2.3653e+06          218.85          3.0878
v  total_pressure       4.8739e+05      6.0482e+05      5.6991e+05      5.5606e+05
v  Local Time Step            0.01        0.034524            0.01        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6595      2.4054e+06          477.92          58.511


 TIME FOR THE TIME STEP              480:        0.17119E+03

===============================================================


 INSTANT    0.481000000E+02   TIME STEP NUMBER             481
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet         v  Velocity[Z]             -11.611          7.5862        -0.72884      -0.0092174
v  ǁVelocityǁ             0.017549          14.707          4.2331          5.0383
v  Pressure                 -12615      1.0482e+05           69908           56056
v  k                    7.9842e-08          2.7805        0.041727        0.047374
v  epsilon               0.0015671      3.7548e+05           615.2          29.289
v  TurbVisc             2.5585e-14         0.32658       0.0022914        0.026375
v  CourantNb              0.068676      2.0466e+05          259.07          55.424
v  FourierNb               0.22433      2.3653e+06          218.85          3.0878
v  total_pressure       4.8739e+05      6.0482e+05      5.6991e+05      5.5606e+05
v  Local Time Step            0.01        0.034524            0.01        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6595      2.4054e+06          477.92          58.511


 TIME FOR THE TIME STEP              480:        0.18590E+03

===============================================================


 INSTANT    0.481000000E+02   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        -0.785727397E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245759E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10208E+02 0.40018E+01
   Friction velocity        uet   :  0.38688E-01 0.25464E+02
   Friction velocity        uk    :  0.42353E-01 0.25464E+02
   Dimensionless distance   yplus :  0.22802E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9316
   Nb of faces within the viscous sub-layer     :      15162
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24156E+01     573   0.24361E+00   0.32566E+01 0.34599E+01 
c  Velocity[X]                                      0.11266E+01 
c  Velocity[Y]                                      0.13049E+01 
c  Velocity[Z]                                      0.82519E+00 
c  Pressure     0.81007E-01     843   0.11522E-01   0.30468E-01 0.28402E-01 
c  k            0.16449E+00     158   0.26886E-03   0.78502E-03 0.30546E+01 
c  epsilon      0.14741E+04     118   0.63186E-03   0.27808E+06 0.16015E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00061681                           108
a  epsilon                 -9.9389                           161
a  Local Time Step      3.5467e-08                        281768


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.5513          10.197          1.1287          0.2629
v  Velocity[Y]             -8.6381           12.85         0.92644         0.62273
v  Velocity[Z]             -11.782          8.2432        -0.71665      -0.0094345
v  ǁVelocityǁ             0.013123          14.615          4.2231          5.0378
v  Pressure                 -12556       1.048e+05           69895           56051
v  k                    8.7108e-08           2.797        0.041503        0.047373
v  epsilon               0.0018671      3.7906e+05          606.72          29.378
v  TurbVisc             5.4907e-13         0.32658       0.0022603        0.026379
v  CourantNb              0.004095      2.8195e+05          261.01          55.486
v  FourierNb               0.22421      2.3653e+06          218.77          3.0886
v  total_pressure       4.8744e+05       6.048e+05      5.6989e+05      5.5605e+05
v  Local Time Step            0.01        0.037976        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6531      2.4074e+06          479.78          58.575


 TIME FOR THE TIME STEP              481:        0.17405E+03

===============================================================


 INSTANT    0.482000000E+02   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        -0.207802021E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245960E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10202E+02 0.40123E+01
   Friction velocity        uet   :  0.19696E-01 0.55816E+02
   Friction velocity        uk    :  0.38425E-01 0.55816E+02
   Dimensionless distance   yplus :  0.28318E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9292
   Nb of faces within the viscous sub-layer     :      15313
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24170E+01     569   0.23681E+00   0.35874E+01 0.36300E+01 
c  Velocity[X]                                      0.10766E+01 
c  Velocity[Y]                                      0.16817E+01 
c  Velocity[Z]                                      0.82915E+00 
c  Pressure     0.81228E-01     799   0.11345E-01   0.30556E-01 0.39188E-01 
c  k            0.16447E+00     177   0.22974E-03   0.80495E-03 0.30919E+01 
c  epsilon      0.14722E+04      93   0.70654E-03   0.18453E+06 0.13123E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0017884                            83
a  epsilon                 -22.983                           155
a  Local Time Step      2.4951e-08                        281763


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.7223          10.199          1.1276         0.26341
v  Velocity[Y]              -8.639          13.195         0.90343          0.6232
v  Velocity[Z]             -12.004          8.0906        -0.69962      -0.0099276
v  ǁVelocityǁ            0.0056919          15.017          4.2049          5.0399
v  Pressure                 -12511      1.0482e+05           69900           56068
v  k                    4.4434e-09          2.7718        0.041243         0.04737
v  epsilon              0.00015636      3.7391e+05          597.12          29.171
v  TurbVisc             6.4221e-13         0.32658       0.0022595        0.026378
v  CourantNb              0.069135      4.0078e+05          261.13          55.453
v  FourierNb               0.22404      2.3653e+06          218.75          3.0882
v  total_pressure       4.8749e+05      6.0482e+05       5.699e+05      5.5607e+05
v  Local Time Step            0.01        0.041774        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6518      2.5264e+06          479.88          58.542


 TIME FOR THE TIME STEP              482:        0.16909E+03

===============================================================


 INSTANT    0.483000000E+02   TIME STEP NUMBER             483
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
----------------------------------------------Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245965E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10198E+02 0.40044E+01
   Friction velocity        uet   :  0.19199E-01 0.56652E+02
   Friction velocity        uk    :  0.19283E-01 0.56652E+02
   Dimensionless distance   yplus :  0.39053E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9287
   Nb of faces within the viscous sub-layer     :      15226
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24194E+01     565   0.24241E+00   0.35007E+01 0.35867E+01 
c  Velocity[X]                      Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245965E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10198E+02 0.40044E+01
   Friction velocity        uet   :  0.19199E-01 0.56652E+02
   Friction velocity        uk    :  0.19283E-01 0.56652E+02
   Dimensionless distance   yplus :  0.39053E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9287
   Nb of faces within the viscous sub-layer     :      15226
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24194E+01     565   0.24241E+00   0.35007E+01 0.35867E+01 
c  Velocity[X]                       Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245965E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10198E+02 0.40044E+01
   Friction velocity        uet   :  0.19199E-01 0.56652E+02
   Friction velocity        uk    :  0.19283E-01 0.56652E+02
   Dimensionless distance   yplus :  0.39053E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9287
   Nb of faces within the viscous sub-layer     :      15226
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24194E+01     565   0.24241E+00   0.35007E+01 0.35867E+01 
c  Velocity[X]                       Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245965E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10198E+02 0.40044E+01
   Friction velocity        uet   :  0.19199E-01 0.56652E+02
   Friction velocity        uk    :  0.19283E-01 0.56652E+02
   Dimensionless distance   yplus :  0.39053E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9287
   Nb of faces within the viscous sub-layer     :      15226
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24194E+01     565   0.24241E+00   0.35007E+01 0.35867E+01 
c  Velocity[X]                                      0.96760E+00 
c  Velocity[Y]                                      0.17127E+01 
c  Velocity[Z]                                      0.82040E+00 
c  Pressure     0.77328E-01     836   0.10938E-01   0.29152E-01 0.31695E-01 
c  k            0.16450E+00     175   0.23455E-03   0.75121E-03 0.29825E+01 
c  epsilon      0.14701E+04     106   0.62547E-03   0.25612E+06 0.15346E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -3.395e-05                             4
a  epsilon                 -1.1389                             7
a  Local Time Step      4.2278e-08                        281763


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.6663          10.279          1.1133         0.26329
v  Velocity[Y]             -8.6111          13.114         0.92824          0.6222
v  Velocity[Z]             -12.694          8.7656        -0.73559      -0.0093593
v  ǁVelocityǁ             0.012753     v  epsilon              0.00062019      3.8035e+05          604.71          29.473
v  TurbVisc             5.1248e-13         0.32658        0.002297        0.026391
v  CourantNb              0.051327      2.9514e+05          261.12          55.488
v  FourierNb               0.22399      2.3653e+06          218.77          3.0908
v  total_pressure        4.876e+05      6.0483e+05      5.6988e+05      5.5606e+05
v  Local Time Step            0.01        0.034961        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6569      2.4206e+06          479.89          58.579


 TIME FOR THE TIME STEP              485:        0.16513E+03

===============================================================


 INSTANT    0.486000000E+02   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        -0.370091416E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245741E+01
Free inlet               13v  epsilon              0.00062019      3.8035e+05          604.71          29.473
v  TurbVisc             5.1248e-13         0.32658        0.002297        0.026391
v  CourantNb              0.051327      2.9514e+05          261.12          55.488
v  FourierNb               0.22399      2.3653e+06          218.77          3.0908
v  total_pressure        4.876e+05      6.0483e+05      5.6988e+05      5.5606e+05
v  Local Time Step            0.01        0.034961        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6569      2.4206e+06          479.89          58.579


 TIME FOR THE TIME STEP              485:        0.17797E+03

===============================================================


 INSTANT    0.486000000E+02   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        -0.370091416E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245741E+01
Free inlet               13 v  epsilon              0.00062019      3.8035e+05          604.71          29.473
v  TurbVisc             5.1248e-13         0.32658        0.002297        0.026391
v  CourantNb              0.051327      2.9514e+05          261.12          55.488
v  FourierNb               0.22399      2.3653e+06          218.77          3.0908
v  total_pressure        4.876e+05      6.0483e+05      5.6988e+05      5.5606e+05
v  Local Time Step            0.01        0.034961        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6569      2.4206e+06          479.89          58.579


 TIME FOR THE TIME STEP              485:        0.18003E+03

===============================================================


 INSTANT    0.486000000E+02   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        -0.370091416E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245741E+01
Free inlet               13 v  epsilon              0.00062019      3.8035e+05          604.71          29.473
v  TurbVisc             5.1248e-13         0.32658        0.002297        0.026391
v  CourantNb              0.051327      2.9514e+05          261.12          55.488
v  FourierNb               0.22399      2.3653e+06          218.77          3.0908
v  total_pressure        4.876e+05      6.0483e+05      5.6988e+05      5.5606e+05
v  Local Time Step            0.01        0.034961        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6569      2.4206e+06          479.89          58.579


 TIME FOR THE TIME STEP              485:        0.16447E+03

===============================================================


 INSTANT    0.486000000E+02   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        -0.370091416E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245741E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10142E+02 0.40138E+01
   Friction velocity        uet   :  0.37030E-01 0.58402E+02
   Friction velocity        uk    :  0.38256E-01 0.58402E+02
   Dimensionless distance   yplus :  0.27293E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9306
   Nb of faces within the viscous sub-layer     :      15270
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24198E+01     561   0.24327E+00   0.40102E+01 0.38388E+01 
c  Velocity[X]                                      0.11539E+01 
c  Velocity[Y]                                      0.19551E+01 
c  Velocity[Z]                                      0.90120E+00 
c  Pressure     0.80640E-01     943   0.11200E-01   0.30412E-01 0.58587E-01 
c  k            0.16455E+00     184   0.24716E-03   0.83447E-03 0.31397E+01 
c  epsilon      0.14616E+04      97   0.47238E-03   0.17280E+06 0.12760E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                      -0.00182                           103
a  epsilon                 -24.357                           184
a  Local Time Step      2.3622e-08                        281760


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.7437          10.331          1.1326         0.26228
v  Velocity[Y]             -8.6471          13.277         0.89506         0.62373
v  Velocity[Z]             -13.019          8.3594        -0.69842        -0.00951
v  ǁVelocityǁ            0.0081447          15.067          4.2031          5.0384
v  Pressure                 -12305      1.0487e+05           69913           56093
v  k                    8.7382e-09          2.7877        0.041652        0.047563
v  epsilon                1.32e-05      3.7717e+05          594.32           29.31
v  TurbVisc             6.0198e-13         0.32658        0.002327        0.026402
v  CourantNb               0.12859      4.2333e+05          261.07          55.473
v  FourierNb               0.22405      2.3653e+06           218.8           3.093
v  total_pressure       4.8769e+05      6.0487e+05      5.6991e+05      5.5609e+05
v  Local Time Step            0.01        0.038457        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4993      2.5489e+06          479.87          58.566


 TIME FOR THE TIME STEP              486:        0.18065E+03

===============================================================


 INSTANT    0.487000000E+02   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        -0.150720917E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245745E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10109E+02 0.39732E+01
   Friction velocity        uet   :  0.35877E-01 0.55725E+02
   Friction velocity        uk    :  0.35862E-01 0.55725E+02
   Dimensionless distance   yplus :  0.49045E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9310
   Nb of faces within the viscous sub-layer     :      15349
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24184E+01     525   0.24497E+00   0.38692E+01 0.37725E+01 
c  Velocity[X]                                      0.11996E+01 
c  Velocity[Y]                                      0.16192E+01 
c  Velocity[Z]                                      0.10504E+01 
c  Pressure     0.85119E-01     973   0.11774E-01   0.32141E-01 0.54755E-01 
c  k            0.16456E+00     206   0.27964E-03   0.75588E-03 0.29860E+01 
c  epsilon      0.14523E+04     104   0.69821E-03   0.26995E+06 0.15948E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00087183                            46
a  epsilon                 -5.2626                            80
a  Local Time Step      4.2278e-08                        281765


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.4403          10.284          1.1115          0.2631
v  Velocity[Y]             -8.6126           12.96         0.89216         0.62389
v  Velocity[Z]             -11.755          7.6922        -0.71942      -0.0089454
v  ǁVelocityǁ             0.010841          14.657          4.2185           5.036
v  Pressure                 -12188      1.0494e+05           69959           56120
v  k                    5.7121e-09           2.784        0.041478        0.047599
v  epsilon              7.6081e-05      3.7591e+05          597.06          29.297
v  TurbVisc             6.5878e-13         0.32658       0.0023969        0.026414
v  CourantNb              0.066785      1.4991e+05          257.11          55.465
v  FourierNb               0.22411      2.3653e+06          218.88           3.096
v  total_pressure       4.8781e+05      6.0494e+05      5.6996e+05      5.5612e+05
v  Local Time Step            0.01        0.042303        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6694      2.4271e+06          475.99          58.561


 TIME FOR THE TIME STEP              487:        0.19506E+03

===============================================================


 INSTANT    0.488000000E+02   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        -0.139823387E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0       Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10134E+02 0.39977E+01
   Friction velocity        uet   :  0.38568E-01 0.31450E+02
   Friction velocity        uk    :  0.38063E-01 0.31450E+02
   Dimensionless distance   yplus :  0.33531E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9333
   Nb of faces within the viscous sub-layer     :      15165
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24199E+01     604   0.24515E+00   0.39846E+01 0.38278E+01 
c  Velocity[X]                                      0.13806E+01 
c  Velocity[Y]                                      0.15695E+01 
c  Velocity[Z]                                      0.10345E+01 
c  Pressure     0.88371E-01    1050   0.12374E-01   0.33365E-01 0.11125E+00 
c  k            0.16Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10134E+02 0.39977E+01
   Friction velocity        uet   :  0.38568E-01 0.31450E+02
   Friction velocity        uk    :  0.38063E-01 0.31450E+02
   Dimensionless distance   yplus :  0.33531E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9333
   Nb of faces within the viscous sub-layer     :      15165
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24199E+01     604   0.24515E+00   0.39846E+01 0.38278E+01 
c  Velocity[X]                                      0.13806E+01 
c  Velocity[Y]                                      0.15695E+01 
c  Velocity[Z]                                      0.10345E+01 
c  Pressure     0.88371E-01    1050   0.12374E-01   0.33365E-01 0.11125E+00 
c  k            0.164Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10134E+02 0.39977E+01
   Friction velocity        uet   :  0.38568E-01 0.31450E+02
   Friction velocity        uk    :  0.38063E-01 0.31450E+02
   Dimensionless distance   yplus :  0.33531E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9333
   Nb of faces within the viscous sub-layer     :      15165
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24199E+01     604   0.24515E+00   0.39846E+01 0.38278E+01 
c  Velocity[X]                                      0.13806E+01 
c  Velocity[Y]                                      0.15695E+01 
c  Velocity[Z]                                      0.10345E+01 
c  Pressure     0.88371E-01    1050   0.12374E-01   0.33365E-01 0.11125E+00 
c  k            0.164Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10134E+02 0.39977E+01
   Friction velocity        uet   :  0.38568E-01 0.31450E+02
   Friction velocity        uk    :  0.38063E-01 0.31450E+02
   Dimensionless distance   yplus :  0.33531E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9333
   Nb of faces within the viscous sub-layer     :      15165
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24199E+01     604   0.24515E+00   0.39846E+01 0.38278E+01 
c  Velocity[X]                                      0.13806E+01 
c  Velocity[Y]                                      0.15695E+01 
c  Velocity[Z]                                      0.10345E+01 
c  Pressure     0.88371E-01    1050   0.12374E-01   0.33365E-01 0.11125E+00 
c  k            0.16463E+00     173   0.36325E-03   0.10539E-02 0.35198E+01 
c  epsilon      0.14644E+04     111   0.67558E-03   0.29299E+06 0.16493E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00064944                           109
a  epsilon                 -9.4601                           149
a  Local Time Step      3.1592e-08                        281765


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.6388          10.248          1.1327         0.26111
v  Velocity[Y]             -8.6965           13.06          0.9222         0.62357
v  Velocity[Z]             -11.873          9.1268        -0.71871      -0.0090747
v  ǁVelocityǁ             0.014755          14.899          4.2248           5.037
v  Pressure                 -11902      1.0511e+05           70122           56250
v  k                    7.7666e-08          2.8168        0.042232         0.04773
v  epsilon              0.00038062     v  FourierNb               0.22437      2.3653e+06          218.83          3.0995
v  total_pressure       4.8816e+05      6.0514e+05      5.7014e+05      5.5626e+05
v  Local Time Step            0.01        0.056305        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6386      2.5765e+06           480.4          58.601


 TIME FOR THE TIME STEP              490:        0.16934E+03

===============================================================


 INSTANT    0.491000000E+02   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        -0.295374343E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245744E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
--------------------v  FourierNb               0.22437      2.3653e+06          218.83          3.0995
v  total_pressure       4.8816e+05      6.0514e+05      5.7014e+05      5.5626e+05
v  Local Time Step            0.01        0.056305        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6386      2.5765e+06           480.4          58.601


 TIME FOR THE TIME STEP              490:        0.17339E+03

===============================================================


 INSTANT    0.491000000E+02   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        -0.295374343E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245744E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------v  FourierNb               0.22437      2.3653e+06          218.83          3.0995
v  total_pressure       4.8816e+05      6.0514e+05      5.7014e+05      5.5626e+05
v  Local Time Step            0.01        0.056305        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6386      2.5765e+06           480.4          58.601


 TIME FOR THE TIME STEP              490:        0.16953E+03

===============================================================


 INSTANT    0.491000000E+02   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        -0.295374343E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245744E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------v  FourierNb               0.22437      2.3653e+06          218.83          3.0995
v  total_pressure       4.8816e+05      6.0514e+05      5.7014e+05      5.5626e+05
v  Local Time Step            0.01        0.056305        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6386      2.5765e+06           480.4          58.601


 TIME FOR THE TIME STEP              490:        0.17051E+03

===============================================================


 INSTANT    0.491000000E+02   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        -0.295374343E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245744E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99971E+01 0.39583E+01
   Friction velocity        uet   :  0.37204E-01 0.57407E+02
   Friction velocity        uk    :  0.42426E-01 0.57407E+02
   Dimensionless distance   yplus :  0.37046E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9291
   Nb of faces within the viscous sub-layer     :      15364
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24130E+01     538   0.24079E+00   0.41044E+01 0.38860E+01 
c  Velocity[X]                                      0.13082E+01 
c  Velocity[Y]                                      0.17354E+01 
c  Velocity[Z]                                      0.10608E+01 
c  Pressure     0.82950E-01     968   0.11413E-01   0.31407E-01 0.64166E-01 
c  k            0.16459E+00     216   0.44598E-03   0.10601E-02 0.35207E+01 
c  epsilon      0.14367E+04      97   0.76264E-03   0.29452E+06 0.16813E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0020797                            77
a  epsilon                 -21.983                           136
a  Local Time Step      4.2278e-08                        281765


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.4928          10.182          1.1095         0.26177
v  Velocity[Y]             -8.6284           13.02         0.89037         0.62397
v  Velocity[Z]             -11.759          8.3594        -0.70861      -0.0089633
v  ǁVelocityǁ             0.013056          14.762          4.2138          5.0364
v  Pressure                 -11844      1.0512e+05           70105           56227
v  k                    4.2539e-08          2.7813        0.041818        0.047786
v  epsilon              0.00045178      3.7411e+05          590.38          29.293
v  TurbVisc             3.3519e-14         0.32658       0.0025473         0.02646
v  CourantNb                0.1315      1.4949e+05          256.46          55.453
v  FourierNb               0.22435      2.3653e+06          218.96          3.1066
v  total_pressure       4.8816e+05      6.0512e+05      5.7011e+05      5.5623e+05
v  Local Time Step            0.01        0.040851        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6404      2.4101e+06          475.43           58.56


 TIME FOR THE TIME STEP              491:        0.17146E+03

===============================================================


 INSTANT    0.492000000E+02   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        -0.288764346E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245953E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
----------------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0010455                            11
a  epsilon                 -6.7616                             9
a  Local Time Step      4.2278e-08                        281764


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.7215          10.232          1.1118         0.26078
v  Velocity[Y]             -8.6751          13.091         0.92803         0.62249
v  Velocity[Z]             -12.304          7.7172        -0.73094      -0.0089243
v  ǁVelocityǁ             0.015629          14.835          4.2352          5.0386
v  Pressure                 -11887      1.0507e+05           70048           56185
v  k                    7.4141e-08          2.7483        0.042436        0.047881
v  epsilon               0.0016153      3.7078e+05          603.76          29.564
v  TurbVisc             1.1785e-13         0.32658       0.0024893        0.026462
v  CourantNb               0.13625      2.1955e+05          258.55          55.445
v  FourierNb               0.22435      2.3653e+06          218.88          3.1038
v  total_pressure       4.8811e+05      6.0507e+05      5.7005e+05      5.5619e+05
v  Local Time Step           -----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0010455                            11
a  epsilon                 -6.7616                             9
a  Local Time Step      4.2278e-08                        281764


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.7215          10.232          1.1118         0.26078
v  Velocity[Y]             -8.6751          13.091         0.92803         0.62249
v  Velocity[Z]             -12.304          7.7172        -0.73094      -0.0089243
v  ǁVelocityǁ             0.015629          14.835          4.2352          5.0386
v  Pressure                 -11887      1.0507e+05           70048           56185
v  k                    7.4141e-08          2.7483        0.042436        0.047881
v  epsilon               0.0016153      3.7078e+05          603.76          29.564
v  TurbVisc             1.1785e-13         0.32658       0.0024893        0.026462
v  CourantNb               0.13625      2.1955e+05          258.55          55.445
v  FourierNb               0.22435      2.3653e+06          218.88          3.1038
v  total_pressure       4.8811e+05      6.0507e+05      5.7005e+05      5.5619e+05
v  Local Time Step            0.01        0.044936        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4744      2.4329e+06          477.44          58.549


 TIME FOR THE TIME STEP              492:        0.17953E+03

===============================================================


 INSTANT    0.493000000E+02   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         0.360445718E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245963E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefi------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98190E+01 0.40338E+01
   Friction velocity        uet   :  0.31687E-01 0.63342E+02
   Friction velocity        uk    :  0.31287E-01 0.63342E+02
   Dimensionless distance   yplus :  0.33342E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9272
   Nb of faces within the viscous sub-layer     :      15330
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24134E+01     587   0.24152E+00   0.42790E+01 0.39675E+01 
c  Velocity[X]                                      0.11674E+01 
c  Velocity[Y]                                      0.21427E+01 
c  Velocity[Z]                                      0.96888E+00 
c  Pressure     0.88547E-01     962   0.12690E-01   0.33587E-01 0.51544E-01 
c  k            0.16476E+00     208   0.65375E-03   0.28310E-02 0.57199E+01 
c  epsilon      0.14587E+04     108   0.62493E-03   0.24274E+06 0.15139E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     ---------------------------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98190E+01 0.40338E+01
   Friction velocity        uet   :  0.31687E-01 0.63342E+02
   Friction velocity        uk    :  0.31287E-01 0.63342E+02
   Dimensionless distance   yplus :  0.33342E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9272
   Nb of faces within the viscous sub-layer     :      15330
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24134E+01     587   0.24152E+00   0.42790E+01 0.39675E+01 
c  Velocity[X]                                      0.11674E+01 
c  Velocity[Y]                                      0.21427E+01 
c  Velocity[Z]                                      0.96888E+00 
c  Pressure     0.88547E-01     962   0.12690E-01   0.33587E-01 0.51544E-01 
c  k            0.16476E+00     208   0.65375E-03   0.28310E-02 0.57199E+01 
c  epsilon      0.14587E+04     108   0.62493E-03   0.24274E+06 0.15139E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     ----------------------------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98190E+01 0.40338E+01
   Friction velocity        uet   :  0.31687E-01 0.63342E+02
   Friction velocity        uk    :  0.31287E-01 0.63342E+02
   Dimensionless distance   yplus :  0.33342E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9272
   Nb of faces within the viscous sub-layer     :      15330
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24134E+01     587   0.24152E+00   0.42790E+01 0.39675E+01 
c  Velocity[X]                                      0.11674E+01 
c  Velocity[Y]                                      0.21427E+01 
c  Velocity[Z]                                      0.96888E+00 
c  Pressure     0.88547E-01     962   0.12690E-01   0.33587E-01 0.51544E-01 
c  k            0.16476E+00     208   0.65375E-03   0.28310E-02 0.57199E+01 
c  epsilon      0.14587E+04     108   0.62493E-03   0.24274E+06 0.15139E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     ----------------------------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98190E+01 0.40338E+01
   Friction velocity        uet   :  0.31687E-01 0.63342E+02
   Friction velocity        uk    :  0.31287E-01 0.63342E+02
   Dimensionless distance   yplus :  0.33342E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9272
   Nb of faces within the viscous sub-layer     :      15330
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24134E+01     587   0.24152E+00   0.42790E+01 0.39675E+01 
c  Velocity[X]                                      0.11674E+01 
c  Velocity[Y]                                      0.21427E+01 
c  Velocity[Z]                                      0.96888E+00 
c  Pressure     0.88547E-01     962   0.12690E-01   0.33587E-01 0.51544E-01 
c  k            0.16476E+00     208   0.65375E-03   0.28310E-02 0.57199E+01 
c  epsilon      0.14587E+04     108   0.62493E-03   0.24274E+06 0.15139E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0023204                           113
a  epsilon                 -36.338                           206
a  Local Time Step      2.1597e-08                        281769


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -5.676          10.367          1.1261         0.26031
v  Velocity[Y]             -8.6119          13.386         0.89248          0.6231
v  Velocity[Z]             -12.801          7.9234        -0.69384      -0.0093758
v  ǁVelocityǁ            0.0099802          15.179          4.1964          5.0358
v  Pressure                 -11908      1.0498e+05           69948           56111
v  k                    4.8267e-09          2.8136        0.042667        0.048095
v  epsilon               7.137e-06      3.8196e+05          588.57          29.475
v  TurbVisc             7.1545e-13         0.32658       0.0024921        0.026491
v  CourantNb               0.25432      4.6302e+05           261.4          55.485
v  FourierNb               0.22476      2.3653e+06          218.85          3.1064
v  total_pressure 
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6787      2.4352e+06          475.37          58.552


 TIME FOR THE TIME STEP              495:        0.17106E+03

===============================================================


 INSTANT    0.496000000E+02   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        -0.250480899E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245959E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
---------------------------------------------------------
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6787      2.4352e+06          475.37          58.552


 TIME FOR THE TIME STEP              495:        0.17269E+03

===============================================================


 INSTANT    0.496000000E+02   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        -0.250480899E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245959E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
----------------------------------------------------------
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6787      2.4352e+06          475.37          58.552


 TIME FOR THE TIME STEP              495:        0.17780E+03

===============================================================


 INSTANT    0.496000000E+02   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        -0.250480899E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245959E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
----------------------------------------------------------
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6787      2.4352e+06          475.37          58.552


 TIME FOR THE TIME STEP              495:        0.17005E+03

===============================================================


 INSTANT    0.496000000E+02   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        -0.250480899E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245959E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.97971E+01 0.39587E+01
   Friction velocity        uet   :  0.37519E-01 0.53291E+02
   Friction velocity        uk    :  0.37040E-01 0.53291E+02
   Dimensionless distance   yplus :  0.40844E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9314
   Nb of faces within the viscous sub-layer     :      15259
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24184E+01     584   0.24152E+00   0.44103E+01 0.40260E+01 
c  Velocity[X]                                      0.12084E+01 
c  Velocity[Y]                                      0.21646E+01 
c  Velocity[Z]                                      0.10373E+01 
c  Pressure     0.85576E-01     956   0.12015E-01   0.32414E-01 0.54754E-01 
c  k            0.16477E+00     205   0.64828E-03   0.21079E-02 0.49348E+01 
c  epsilon      0.14467E+04     115   0.65803E-03   0.27280E+06 0.16081E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00036374                            45
a  epsilon                 -7.8696                            60
a  Local Time Step      4.2278e-08                        281764


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.6938          10.351          1.1128         0.26125
v  Velocity[Y]             -8.6549          13.199         0.92623         0.62183
v  Velocity[Z]             -12.018          7.5275        -0.73487      -0.0086677
v  ǁVelocityǁ             0.014844          14.916          4.2374          5.0384
v  Pressure                 -11656        1.05e+05           69960           56127
v  k                    3.9602e-08          2.7586        0.042538        0.048228
v  epsilon               0.0017131      3.7005e+05          600.42          29.713
v  TurbVisc             1.2417e-13         0.32658       0.0025828        0.026529
v  CourantNb              0.059765      2.2156e+05          258.44          55.467
v  FourierNb               0.22544      2.3653e+06          219.12          3.1114
v  total_pressure       4.8834e+05        6.05e+05      5.6996e+05      5.5613e+05
v  Local Time Step            0.01        0.040984        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6838      2.4314e+06          477.56          58.578


 TIME FOR THE TIME STEP              496:        0.17261E+03

===============================================================


 INSTANT    0.497000000E+02   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        -0.201713264E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245759E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
---------------------------------------------a  k                   -0.00094512                           120
a  epsilon                 -10.459                           182
a  Local Time Step      3.0085e-08                        281767


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.6595          10.268          1.1312         0.26051
v  Velocity[Y]             -8.6295          13.249         0.91974         0.62239
v  Velocity[Z]             -11.603          7.8865        -0.71707      -0.0090153
v  ǁVelocityǁ              0.01587          15.058          4.2263          5.0363
v  Pressure                 -11514      1.0502e+05           69982           56145
v  k                    3.2457e-08          2.7963        0.042744        0.048295
v  epsilon              0.00078432       3.791e+05           598.4          29.814
v  TurbVisc             4.8192e-13         0.32658       0.0025622        0.026549
v  CourantNb             0.0067849      3.3239e+05          261.23          55.559
v  FourierNb               0.22559      2.3653e+06          218.83          3.1124
v  total_pressure       4.8849e+05      6.0502e+05      5.6998e+05      5.5615e+05
v  Local Time Step            0.01        0.045083        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6a  k                   -0.00094512                           120
a  epsilon                 -10.459                           182
a  Local Time Step      3.0085e-08                        281767


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.6595          10.268          1.1312         0.26051
v  Velocity[Y]             -8.6295          13.249         0.91974         0.62239
v  Velocity[Z]             -11.603          7.8865        -0.71707      -0.0090153
v  ǁVelocityǁ              0.01587          15.058          4.2263          5.0363
v  Pressure                 -11514      1.0502e+05           69982           56145
v  k                    3.2457e-08          2.7963        0.042744        0.048295
v  epsilon              0.00078432       3.791e+05           598.4          29.814
v  TurbVisc             4.8192e-13         0.32658       0.0025622        0.026549
v  CourantNb             0.0067849      3.3239e+05          261.23          55.559
v  FourierNb               0.22559      2.3653e+06          218.83          3.1124
v  total_pressure       4.8849e+05      6.0502e+05      5.6998e+05      5.5615e+05
v  Local Time Step            0.01        0.045083        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6712      2.4579e+06          480.06          58.671


 TIME FOR THE TIME STEP              497:        0.18693E+03

===============================================================


 INSTANT    0.498000000E+02   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        -0.595259994E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245748E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
----------------------------------   Dimensionless distance   yplus :  0.60790E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9319
   Nb of faces within the viscous sub-layer     :      15367
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24179E+01     571   0.24663E+00   0.44355E+01 0.40389E+01 
c  Velocity[X]                                      0.14138E+01 
c  Velocity[Y]                                      0.19339E+01 
c  Velocity[Z]                                      0.10878E+01 
c  Pressure     0.86291E-01    1015   0.11601E-01   0.32674E-01 0.73004E-01 
c  k            0.16472E+00     249   0.94004E-03   0.20213E-02 0.48079E+01 
c  epsilon      0.14509E+04     113   0.71287E-03   0.26348E+06 0.15821E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0018085                            51
a  epsilon                 -19.635                            88
a  Local Time Step      4.2278e-08                        281766


    Dimensionless distance   yplus :  0.60790E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9319
   Nb of faces within the viscous sub-layer     :      15367
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24179E+01     571   0.24663E+00   0.44355E+01 0.40389E+01 
c  Velocity[X]                                      0.14138E+01 
c  Velocity[Y]                                      0.19339E+01 
c  Velocity[Z]                                      0.10878E+01 
c  Pressure     0.86291E-01    1015   0.11601E-01   0.32674E-01 0.73004E-01 
c  k            0.16472E+00     249   0.94004E-03   0.20213E-02 0.48079E+01 
c  epsilon      0.14509E+04     113   0.71287E-03   0.26348E+06 0.15821E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0018085                            51
a  epsilon                 -19.635                            88
a  Local Time Step      4.2278e-08                        281766


     Dimensionless distance   yplus :  0.60790E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9319
   Nb of faces within the viscous sub-layer     :      15367
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24179E+01     571   0.24663E+00   0.44355E+01 0.40389E+01 
c  Velocity[X]                                      0.14138E+01 
c  Velocity[Y]                                      0.19339E+01 
c  Velocity[Z]                                      0.10878E+01 
c  Pressure     0.86291E-01    1015   0.11601E-01   0.32674E-01 0.73004E-01 
c  k            0.16472E+00     249   0.94004E-03   0.20213E-02 0.48079E+01 
c  epsilon      0.14509E+04     113   0.71287E-03   0.26348E+06 0.15821E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0018085                            51
a  epsilon                 -19.635                            88
a  Local Time Step      4.2278e-08                        281766


     Dimensionless distance   yplus :  0.60790E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9319
   Nb of faces within the viscous sub-layer     :      15367
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24179E+01     571   0.24663E+00   0.44355E+01 0.40389E+01 
c  Velocity[X]                                      0.14138E+01 
c  Velocity[Y]                                      0.19339E+01 
c  Velocity[Z]                                      0.10878E+01 
c  Pressure     0.86291E-01    1015   0.11601E-01   0.32674E-01 0.73004E-01 
c  k            0.16472E+00     249   0.94004E-03   0.20213E-02 0.48079E+01 
c  epsilon      0.14509E+04     113   0.71287E-03   0.26348E+06 0.15821E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0018085                            51
a  epsilon                 -19.635                            88
a  Local Time Step      4.2278e-08                        281766


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.4617          10.134           1.118         0.26253
v  Velocity[Y]             -8.6793          12.922         0.87621         0.62441
v  Velocity[Z]             -11.616          7.6479        -0.70707      -0.0088416
v  ǁVelocityǁ             0.016732           14.64          4.2071           5.037
v  Pressure                 -11284      1.0511e+05           70052           56197
v  k                    1.7207e-08          2.7935        0.043229         0.04841
v  epsilon              0.00051227      3.7737e+05          590.52          29.631
v  TurbVisc             3.5996e-13         0.32658       0.0029308        0.026597
v  CourantNb              0.044899      1.4226e+05          257.17          55.478
v  FourierNb               0.22531      2.3653e+06          219.23          3.1319
v  total_pressure       4.8872e+05      6.0511e+05      5.7005e+05       5.562e+05
v  Local Time Step            0.01        0.042664        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
    INSTANT    0.501000000E+02   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        -0.180422249E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245745E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99381E+01 0.39592E+01
   Friction velocity        uet   :  0.39464E-01 0.34782E+02
   Friction velocity        uk    :  0.39373E-01 0.34782E+02
   Dimensionless distance   yplus :  0.44382E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9334
   Nb of face INSTANT    0.501000000E+02   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        -0.180422249E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245745E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99381E+01 0.39592E+01
   Friction velocity        uet   :  0.39464E-01 0.34782E+02
   Friction velocity        uk    :  0.39373E-01 0.34782E+02
   Dimensionless distance   yplus :  0.44382E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9334
   Nb of faces INSTANT    0.501000000E+02   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        -0.180422249E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245745E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99381E+01 0.39592E+01
   Friction velocity        uet   :  0.39464E-01 0.34782E+02
   Friction velocity        uk    :  0.39373E-01 0.34782E+02
   Dimensionless distance   yplus :  0.44382E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9334
   Nb of faces INSTANT    0.501000000E+02   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        -0.180422249E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245745E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99381E+01 0.39592E+01
   Friction velocity        uet   :  0.39464E-01 0.34782E+02
   Friction velocity        uk    :  0.39373E-01 0.34782E+02
   Dimensionless distance   yplus :  0.44382E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9334
   Nb of faces within the viscous sub-layer     :      15227
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27612E+01     731   0.21265E+00   0.69088E+02 0.13983E+02 
c  Velocity[X]                                      0.37850E+01 
c  Velocity[Y]                                      0.67636E+01 
c  Velocity[Z]                                      0.58539E+02 
c  Pressure     0.87069E-01    1735   0.82136E-01   0.32968E-01 0.19361E+02 
c  k            0.30834E+00     302   0.16625E-02   0.22332E+00 0.34191E+02 
c  epsilon      0.14330E+04     180   0.87285E-03   0.39404E+06 0.19673E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0007366                           110
a  epsilon                 -130.91                           165
a  Local Time Step       2.886e-08                        281767


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.7043          12.012          1.2698         0.30455
v  Velocity[Y]              -9.786          15.852          1.0903         0.71913
v  Velocity[Z]             -14.972          8.3201        -0.74207        0.023527
v  ǁVelocityǁ             0.029763           19.43          4.5383          5.7439
v  Pressure                -66.435      1.2682e+05           85968           71528
v  k                    6.2945e-08          2.7259         0.04379        0.065969
v  epsilon              0.00033537      3.6765e+05          599.95          32.314
v  TurbVisc             5.1993e-13         0.32658       0.0027332        0.026604
v  CourantNb               0.27592       3.465e+05          259.92          55.522
v  FourierNb               0.22496      2.3653e+06          218.94          3.1254
v  total_pressure       4.9993e+05      6.2682e+05      5.8597e+05      5.7153e+05
v  Local Time Step            0.01        0.046207        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6948       2.472e+06          478.86          58.647


 TIME FOR THE TIME STEP              501:        0.24035E+03

===============================================================


 INSTANT    0.502000000E+02   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        -0.301169417E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969618E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11741E+02 0.44877E+01
   Friction velocity        uet   :  0.23306E-01 0.67085E+02
   Friction velocity        uk    :  0.23069E-01 0.67085E+02
   Dimensionless distance   yplus :  0.66436E-02 0.19744E+02
   ------------------------------------------------------
   Nb of reversal of th-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.6219          11.833          1.2687         0.32458
v  Velocity[Y]              -8.859          16.878          1.1279         0.76964
v  Velocity[Z]             -15.514          9.0222         -0.5174          0.1268
v  ǁVelocityǁ            0.0087581          19.459          4.5193          5.9584
v  Pressure                -91.303      1.3228e+05           93022           75928
v  k                    4.0098e-08          4.2251         0.04986        0.076238
v  epsilon              7.3831e-05      7.1477e+05          877.32          39.724
v  TurbVisc              4.725e-13         0.41625       0.0030235        0.037359
v  CourantNb             0.0060803      4.9186e+05          287.71          64.176
v  FourierNb               0.22546      2.3653e+06           218.8          3.2659
v  total_pressure       4.9991e+05      6.3228e+05      5.9302e+05      5.7593e+05
v  Local Time Step            0.01        0.034589            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0522      2.6174e+06          506.52          67.442


 TIME FOR THE TIME STEP              502:        0.24222E+03

===============================================================


 INSTANT    0.503000000E+02   TIME STEP NUMBER             503
 ============================================================= 




   ** BOUNDARY MASS FLOW INF-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.6219          11.833          1.2687         0.32458
v  Velocity[Y]              -8.859          16.878          1.1279         0.76964
v  Velocity[Z]             -15.514          9.0222         -0.5174          0.1268
v  ǁVelocityǁ            0.0087581          19.459          4.5193          5.9584
v  Pressure                -91.303      1.3228e+05           93022           75928
v  k                    4.0098e-08          4.2251         0.04986        0.076238
v  epsilon              7.3831e-05      7.1477e+05          877.32          39.724
v  TurbVisc              4.725e-13         0.41625       0.0030235        0.037359
v  CourantNb             0.0060803      4.9186e+05          287.71          64.176
v  FourierNb               0.22546      2.3653e+06           218.8          3.2659
v  total_pressure       4.9991e+05      6.3228e+05      5.9302e+05      5.7593e+05
v  Local Time Step            0.01        0.034589            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0522      2.6174e+06          506.52          67.442


 TIME FOR THE TIME STEP              502:        0.23681E+03

===============================================================


 INSTANT    0.503000000E+02   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         0.660466377E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969610E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11741E+02 0.45028E+01
   Friction velocity        uet   :  0.25588E-01 0.59254E+02
   Friction velocity        uk    :  0.25532E-01 0.59254E+02
   Dimensionless distance   yplus :  0.75608E-02 0.20540E+02
   ----------------------------------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34008E+01     717   0.21659E+00   0.99740E+01 0.50594E+01 
c  Velocity[X]                                      0.21571E+01 
c  Velocity[Y]                                      0.41935E+01 
c  Velocity[Z]                                      0.36234E+01 
c  Pressure     0.27022E+00    1521   0.67979E-01   0.98273E-01 0.33482E+01 
c  k            0.31961E+00     238   0.60297E-03   0.85886E-02 0.63294E+01 
c  epsilon      0.19606E+04     135   0.20479E-02   0.22308E+07 0.38814E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0008873                            21
a  epsilon                 -88.186                            41
a  Local Time Step      3.5987e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -5.871          11.921          1.2606         0------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34008E+01     717   0.21659E+00   0.99740E+01 0.50594E+01 
c  Velocity[X]                                      0.21571E+01 
c  Velocity[Y]                                      0.41935E+01 
c  Velocity[Z]                                      0.36234E+01 
c  Pressure     0.27022E+00    1521   0.67979E-01   0.98273E-01 0.33482E+01 
c  k            0.31961E+00     238   0.60297E-03   0.85886E-02 0.63294E+01 
c  epsilon      0.19606E+04     135   0.20479E-02   0.22308E+07 0.38814E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0008873                            21
a  epsilon                 -88.186                            41
a  Local Time Step      3.5987e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -5.871          11.921          1.2606         0.------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34008E+01     717   0.21659E+00   0.99740E+01 0.50594E+01 
c  Velocity[X]                                      0.21571E+01 
c  Velocity[Y]                                      0.41935E+01 
c  Velocity[Z]                                      0.36234E+01 
c  Pressure     0.27022E+00    1521   0.67979E-01   0.98273E-01 0.33482E+01 
c  k            0.31961E+00     238   0.60297E-03   0.85886E-02 0.63294E+01 
c  epsilon      0.19606E+04     135   0.20479E-02   0.22308E+07 0.38814E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0008873                            21
a  epsilon                 -88.186                            41
a  Local Time Step      3.5987e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -5.871          11.921          1.2606         0.------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34008E+01     717   0.21659E+00   0.99740E+01 0.50594E+01 
c  Velocity[X]                                      0.21571E+01 
c  Velocity[Y]                                      0.41935E+01 
c  Velocity[Z]                                      0.36234E+01 
c  Pressure     0.27022E+00    1521   0.67979E-01   0.98273E-01 0.33482E+01 
c  k            0.31961E+00     238   0.60297E-03   0.85886E-02 0.63294E+01 
c  epsilon      0.19606E+04     135   0.20479E-02   0.22308E+07 0.38814E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0008873                            21
a  epsilon                 -88.186                            41
a  Local Time Step      3.5987e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -5.871          11.921          1.2606         0.32004
v  Velocity[Y]             -8.8234          16.131          1.2318         0.76842
v  Velocity[Z]             -13.961          9.4845        -0.75514        0.012359
v  ǁVelocityǁ               0.0234          18.758          4.6625          6.0562
v  Pressure                -5370.2      1.3413e+05           91775           72486
v  k                    1.9624e-08          3.3558         0.04596        0.073666
v  epsilon               0.0030722      5.6435e+05          798.29           37.86
v  TurbVisc             7.5399e-14         0.41837       0.0028647        0.037246
v  CourantNb              0.072601      2.7788e+05          289.53          64.632
v  FourierNb               0.22574      2.3653e+06          218.57          3.2632
v  total_pressure       4.9463e+05      6.3413e+05      5.9177e+05      5.7249e+05
v  Local Time Step            0.01        0.029379            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.1315      2.4688e+06           508.1          67.895


 TIME FOR THE TIME STEP              504:        0.22915E+03

===============================================================


 INSTANT    0.505000000E+02   TIME STEP NUMBER             5Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.105005024E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969857E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12148E+02 0.45023E+01
   Friction velocity        uet   :  0.30464E-01 0.47772E+02
   Friction velocity        uk    :  0.38953E-01 0.47772E+02
   Dimensionless distance   yplus :  0.60958E-02 0.20250E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10716
   Nb of faces within the viscous sub-layer     :      13860
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-------------------------------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.105005024E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969857E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12148E+02 0.45023E+01
   Friction velocity        uet   :  0.30464E-01 0.47772E+02
   Friction velocity        uk    :  0.38953E-01 0.47772E+02
   Dimensionless distance   yplus :  0.60958E-02 0.20250E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10716
   Nb of faces within the viscous sub-layer     :      13860
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
--------------------------------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.105005024E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969857E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12148E+02 0.45023E+01
   Friction velocity        uet   :  0.30464E-01 0.47772E+02
   Friction velocity        uk    :  0.38953E-01 0.47772E+02
   Dimensionless distance   yplus :  0.60958E-02 0.20250E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10716
   Nb of faces within the viscous sub-layer     :      13860
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
--------------------------------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.105005024E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969857E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12148E+02 0.45023E+01
   Friction velocity        uet   :  0.30464E-01 0.47772E+02
   Friction velocity        uk    :  0.38953E-01 0.47772E+02
   Dimensionless distance   yplus :  0.60958E-02 0.20250E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10716
   Nb of faces within the viscous sub-layer     :      13860
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33785E+01     668   0.21668E+00   0.78153E+01 0.44772E+01 
c  Velocity[X]                                      0.18915E+01 
c  Velocity[Y]                                      0.37183E+01 
c  Velocity[Z]                                      0.22055E+01 
c  Pressure     0.23185E+00    1466   0.53297E-01   0.82045E-01 0.20013E+01 
c  k            0.31961E+00     216   0.20940E-03   0.29900E-02 0.37332E+01 
c  epsilon      0.19342E+04     116   0.93568E-03   0.84565E+06 0.24151E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0013227                            62
a  epsilon                 -24.371                           114
a  Local Time Step      2.6832e-08                        281771


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  ---v  Velocity[Z]             -13.835          9.9837        -0.86585       -0.023982
v  ǁVelocityǁ            0.0033857          18.013          4.7551          6.0443
v  Pressure                 -15496      1.3066e+05           86177           68116
v  k                    8.0045e-08          3.1248        0.048295        0.073826
v  epsilon               0.0013064      4.3189e+05          815.99          38.452
v  TurbVisc             4.1548e-13         0.41838       0.0027796        0.037649
v  CourantNb              0.014616      2.2764e+05          294.37          65.406
v  FourierNb                0.2262      2.3653e+06          218.62          3.2597
v  total_pressure        4.845e+05      6.3066e+05      5.8618e+05      5.6812e+05
v  Local Time Step            0.01        0.033891            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2111      2.3867e+06          512.99          68.666


 TIME FOR THE TIME STEP              507:        0.21309E+03

===============================================================


 INSTANT    0.508000000E+02   TIME STEP NUMBER             508
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet        v  Velocity[Z]             -13.835          9.9837        -0.86585       -0.023982
v  ǁVelocityǁ            0.0033857          18.013          4.7551          6.0443
v  Pressure                 -15496      1.3066e+05           86177           68116
v  k                    8.0045e-08          3.1248        0.048295        0.073826
v  epsilon               0.0013064      4.3189e+05          815.99          38.452
v  TurbVisc             4.1548e-13         0.41838       0.0027796        0.037649
v  CourantNb              0.014616      2.2764e+05          294.37          65.406
v  FourierNb                0.2262      2.3653e+06          218.62          3.2597
v  total_pressure        4.845e+05      6.3066e+05      5.8618e+05      5.6812e+05
v  Local Time Step            0.01        0.033891            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2111      2.3867e+06          512.99          68.666


 TIME FOR THE TIME STEP              507:        0.20928E+03

===============================================================


 INSTANT    0.508000000E+02   TIME STEP NUMBER             508
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet         v  Velocity[Z]             -13.835          9.9837        -0.86585       -0.023982
v  ǁVelocityǁ            0.0033857          18.013          4.7551          6.0443
v  Pressure                 -15496      1.3066e+05           86177           68116
v  k                    8.0045e-08          3.1248        0.048295        0.073826
v  epsilon               0.0013064      4.3189e+05          815.99          38.452
v  TurbVisc             4.1548e-13         0.41838       0.0027796        0.037649
v  CourantNb              0.014616      2.2764e+05          294.37          65.406
v  FourierNb                0.2262      2.3653e+06          218.62          3.2597
v  total_pressure        4.845e+05      6.3066e+05      5.8618e+05      5.6812e+05
v  Local Time Step            0.01        0.033891            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2111      2.3867e+06          512.99          68.666


 TIME FOR THE TIME STEP              507:        0.20321E+03

===============================================================


 INSTANT    0.508000000E+02   TIME STEP NUMBER             508
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet         v  Velocity[Z]             -13.835          9.9837        -0.86585       -0.023982
v  ǁVelocityǁ            0.0033857          18.013          4.7551          6.0443
v  Pressure                 -15496      1.3066e+05           86177           68116
v  k                    8.0045e-08          3.1248        0.048295        0.073826
v  epsilon               0.0013064      4.3189e+05          815.99          38.452
v  TurbVisc             4.1548e-13         0.41838       0.0027796        0.037649
v  CourantNb              0.014616      2.2764e+05          294.37          65.406
v  FourierNb                0.2262      2.3653e+06          218.62          3.2597
v  total_pressure        4.845e+05      6.3066e+05      5.8618e+05      5.6812e+05
v  Local Time Step            0.01        0.033891            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2111      2.3867e+06          512.99          68.666


 TIME FOR THE TIME STEP              507:        0.20496E+03

===============================================================


 INSTANT    0.508000000E+02   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        -0.145048958E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969863E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12160E+02 0.45018E+01
   Friction velocity        uet   :  0.28369E-01 0.58789E+02
   Friction velocity        uk    :  0.28343E-01 0.58789E+02
   Dimensionless distance   yplus :  0.75016E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10700
   Nb of faces within the viscous sub-layer     :      13699
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33700E+01     666   0.22303E+00   0.51172E+01 0.36307E+01 
c  Velocity[X]                                      0.12592E+01 
c  Velocity[Y]                                      0.23332E+01 
c  Velocity[Z]                                      0.15249E+01 
c  Pressure     0.19568E+00    1334   0.44185E-01   0.67504E-01 0.11873E+01 
c  k            0.31958E+00     252   0.45153E-03   0.47923E-02 0.47341E+01 
c  epsilon      0.19297E+04     141   0.66053E-03   0.67092E+06 0.20813E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0011969                             8
a  epsilon                 -30.218                            22
a  Local Time Step      3.5733e-08                        281766


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.9904          10.832          1.3026         0.31593
v  Velocity[Y]             -8.8857          15.912          1.1622         0.75688
v  Velocity[Z]             -13.987          9.2462         -0.8472       -0.013826
v  ǁVelocityǁ            0.0021071          18.216          4.7728          6.0394
v  Pressure                 -15836      1.3181e+05           86792           69017
v  k                    1.4038e-07          2.8412        0.047303        0.073585
v  epsilon               0.0014278      3.8778e+05          814.77          38.265
v  TurbVisc             4.6603e-13         0.41838        0.002918        0.037649
v  CourantNb               0.16421      2.7985e+05          295.45          65.447
v  FourierNb               0.22596      2.3653e+06           218.9          3.2638
v  total_pressure       4.8416e+05      6.3181e+05      5.8679e+05      5.6902e+05
v  Local Time Step            0.01        0.033066        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2503        2.39e+06          514.36          68.711


 TIME FOR THE TIME STEP              508:        0.21686E+03

===============================================================


 INSTANT    0.509000000E+02   TIME STEP NUMBER             509
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
-----------------------------------------------------------------------------
c  Velocity     0.33733E+01     653   0.22553E+00   0.46268E+01 0.34503E+01 
c  Velocity[X]                                      0.12591E+01 
c  Velocity[Y]                                      0.21090E+01 
c  Velocity[Z]                                      0.12586E+01 
c  Pressure     0.18698E+00    1411   0.41003E-01   0.63677E-01 0.15915E+01 
c  k            0.31959E+00     196   0.16549E-03   0.16509E-02 0.27799E+01 
c  epsilon      0.18931E+04     114   0.11369E-02   0.59761E+06 0.19959E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0011743                            37
a  epsilon                 -51.856                            58
a  Local Time Step      3.5351e-08                        281767


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.9046          10.742          1.3154         0.31767
v  Velocity[Y]             -8.8484          15.809          1.1485         0.75928
v  Velocity[Z]             -13.866           10.37        -0.82303      -0.0073026
v  ǁVelocityǁ             0.010166          18.086          4.7852           6.041
v  Pressure                 ------------------------------------------------------------------------------
c  Velocity     0.33733E+01     653   0.22553E+00   0.46268E+01 0.34503E+01 
c  Velocity[X]                                      0.12591E+01 
c  Velocity[Y]                                      0.21090E+01 
c  Velocity[Z]                                      0.12586E+01 
c  Pressure     0.18698E+00    1411   0.41003E-01   0.63677E-01 0.15915E+01 
c  k            0.31959E+00     196   0.16549E-03   0.16509E-02 0.27799E+01 
c  epsilon      0.18931E+04     114   0.11369E-02   0.59761E+06 0.19959E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0011743                            37
a  epsilon                 -51.856                            58
a  Local Time Step      3.5351e-08                        281767


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.9046          10.742          1.3154         0.31767
v  Velocity[Y]             -8.8484          15.809          1.1485         0.75928
v  Velocity[Z]             -13.866           10.37        -0.82303      -0.0073026
v  ǁVelocityǁ             0.010166          18.086          4.7852           6.041
v  Pressure                 -15519      1.3349e+05           87971           70330
v  k                    4.1102e-08           2.816        0.047311        0.073505
v  epsilon              0.00056596      3.8282e+05          801.64          38.382
v  TurbVisc             5.1487e-13         0.41838       0.0027306        0.037616
v  CourantNb              0.065535      2.8288e+05          296.56          65.584
v  FourierNb               0.22589      2.3653e+06          218.74          3.2518
v  total_pressure       4.8448e+05      6.3349e+05      5.8797e+05      5.7033e+05
v  Local Time Step            0.01        0.036373        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.3372       2.405e+06           515.3          68.836


 TIME FOR THE TIME STEP              509:        0.21000E+03

===============================================================


 INSTANT    0.510000000E+02   TIME STEP NUMBER             510
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
----------------------------------------------Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969596E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12298E+02 0.45011E+01
   Friction velocity        uet   :  0.18826E-01 0.42541E+02
   Friction velocity        uk    :  0.19023E-01 0.42541E+02
   Dimensionless distance   yplus :  0.28782E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10786
   Nb of faces within the viscous sub-layer     :      13737
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33860E+01     608   0.22128E+00   0.48063E+01 0.35083E+01 
c  Velocity[X]                      Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969596E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12298E+02 0.45011E+01
   Friction velocity        uet   :  0.18826E-01 0.42541E+02
   Friction velocity        uk    :  0.19023E-01 0.42541E+02
   Dimensionless distance   yplus :  0.28782E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10786
   Nb of faces within the viscous sub-layer     :      13737
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33860E+01     608   0.22128E+00   0.48063E+01 0.35083E+01 
c  Velocity[X]                       Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969596E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12298E+02 0.45011E+01
   Friction velocity        uet   :  0.18826E-01 0.42541E+02
   Friction velocity        uk    :  0.19023E-01 0.42541E+02
   Dimensionless distance   yplus :  0.28782E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10786
   Nb of faces within the viscous sub-layer     :      13737
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33860E+01     608   0.22128E+00   0.48063E+01 0.35083E+01 
c  Velocity[X]                       Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969596E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12298E+02 0.45011E+01
   Friction velocity        uet   :  0.18826E-01 0.42541E+02
   Friction velocity        uk    :  0.19023E-01 0.42541E+02
   Dimensionless distance   yplus :  0.28782E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10786
   Nb of faces within the viscous sub-layer     :      13737
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33860E+01     608   0.22128E+00   0.48063E+01 0.35083E+01 
c  Velocity[X]                                      0.12443E+01 
c  Velocity[Y]                                      0.22699E+01 
c  Velocity[Z]                                      0.12922E+01 
c  Pressure     0.17738E+00    1373   0.34980E-01   0.58886E-01 0.13116E+01 
c  k            0.31955E+00     177   0.16684E-03   0.13851E-02 0.25451E+01 
c  epsilon      0.18705E+04     113   0.77365E-03   0.58600E+06 0.19471E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00035538                            56
a  epsilon                 -38.055                           107
a  Local Time Step      4.2278e-08                        281776


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -5.873          10.939          1.3257         0.32095
v  Velocity[Y]             -8.8904          14.901          1.0982         0.76339
v  Velocity[Z]             -13.748          10.481        -0.77734      -0.0056581
v  ǁVelocityǁ            0.0082914     v  epsilon                0.002006      3.8797e+05          787.88          38.222
v  TurbVisc             1.0986e-14         0.41838       0.0027475        0.037603
v  CourantNb               0.32588      2.3731e+05          295.04          65.745
v  FourierNb               0.22676      2.3653e+06          218.85          3.2503
v  total_pressure       4.8562e+05      6.3792e+05      5.9126e+05      5.7346e+05
v  Local Time Step            0.01        0.048413        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6585      2.3716e+06          513.89          68.995


 TIME FOR THE TIME STEP              512:        0.21406E+03

===============================================================


 INSTANT    0.513000000E+02   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        -0.245905319E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969610E+01
Free inlet               13v  epsilon                0.002006      3.8797e+05          787.88          38.222
v  TurbVisc             1.0986e-14         0.41838       0.0027475        0.037603
v  CourantNb               0.32588      2.3731e+05          295.04          65.745
v  FourierNb               0.22676      2.3653e+06          218.85          3.2503
v  total_pressure       4.8562e+05      6.3792e+05      5.9126e+05      5.7346e+05
v  Local Time Step            0.01        0.048413        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6585      2.3716e+06          513.89          68.995


 TIME FOR THE TIME STEP              512:        0.21004E+03

===============================================================


 INSTANT    0.513000000E+02   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        -0.245905319E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969610E+01
Free inlet               13 v  epsilon                0.002006      3.8797e+05          787.88          38.222
v  TurbVisc             1.0986e-14         0.41838       0.0027475        0.037603
v  CourantNb               0.32588      2.3731e+05          295.04          65.745
v  FourierNb               0.22676      2.3653e+06          218.85          3.2503
v  total_pressure       4.8562e+05      6.3792e+05      5.9126e+05      5.7346e+05
v  Local Time Step            0.01        0.048413        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6585      2.3716e+06          513.89          68.995


 TIME FOR THE TIME STEP              512:        0.21238E+03

===============================================================


 INSTANT    0.513000000E+02   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        -0.245905319E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969610E+01
Free inlet               13 v  epsilon                0.002006      3.8797e+05          787.88          38.222
v  TurbVisc             1.0986e-14         0.41838       0.0027475        0.037603
v  CourantNb               0.32588      2.3731e+05          295.04          65.745
v  FourierNb               0.22676      2.3653e+06          218.85          3.2503
v  total_pressure       4.8562e+05      6.3792e+05      5.9126e+05      5.7346e+05
v  Local Time Step            0.01        0.048413        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6585      2.3716e+06          513.89          68.995


 TIME FOR THE TIME STEP              512:        0.20015E+03

===============================================================


 INSTANT    0.513000000E+02   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        -0.245905319E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969610E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           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+02 0.45007E+01
   Friction velocity        uet   :  0.28235E-01 0.46468E+02
   Friction velocity        uk    :  0.27585E-01 0.46468E+02
   Dimensionless distance   yplus :  0.55641E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10802
   Nb of faces within the viscous sub-layer     :      13788
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34018E+01     604   0.22098E+00   0.43773E+01 0.33363E+01 
c  Velocity[X]                                      0.14024E+01 
c  Velocity[Y]                                      0.18344E+01 
c  Velocity[Z]                                      0.11404E+01 
c  Pressure     0.17098E+00    1302   0.30490E-01   0.55297E-01 0.70323E+00 
c  k            0.31951E+00     161   0.11198E-03   0.81890E-03 0.19584E+01 
c  epsilon      0.18478E+04      94   0.43110E-03   0.22671E+06 0.12339E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00095147                            21
a  epsilon                 -74.638                            56
a  Local Time Step      3.7206e-08                        281780


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.9829          11.238          1.3477         0.32081
v  Velocity[Y]             -9.3091          14.778           1.096         0.76473
v  Velocity[Z]             -13.467          10.462        -0.77543      -0.0097295
v  ǁVelocityǁ             0.021532          17.409          4.8192           6.071
v  Pressure                 -14354       1.388e+05           91899           73962
v  k                    1.3658e-07          2.8492        0.046485        0.073393
v  epsilon               0.0020601      3.9291e+05          780.72          38.263
v  TurbVisc              2.022e-13         0.41837       0.0026155         0.03759
v  CourantNb              0.066318      2.6877e+05          295.91          65.889
v  FourierNb               0.22682      2.3653e+06          218.66          3.2437
v  total_pressure       4.8565e+05       6.388e+05       5.919e+05      5.7396e+05
v  Local Time Step            0.01        0.053254        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.3752      2.3942e+06          514.58          69.132


 TIME FOR THE TIME STEP              513:        0.20619E+03

===============================================================


 INSTANT    0.514000000E+02   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        -0.528711875E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3  c  Velocity[Z]                                      0.10318E+01 
c  Pressure     0.16236E+00    1297   0.28357E-01   0.51853E-01 0.57771E+00 
c  k            0.31954E+00     153   0.90948E-04   0.70466E-03 0.18162E+01 
c  epsilon      0.18718E+04      92   0.56264E-03   0.35354E+06 0.15139E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00045797                            41
a  epsilon                 -28.055                            62
a  Local Time Step      3.5881e-08                        281774


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.1365          11.454          1.3476          0.3211
v  Velocity[Y]             -9.4892          15.025          1.0819         0.76585
v  Velocity[Z]             -13.391          9.7888        -0.77355       -0.011438
v  ǁVelocityǁ             0.018501          17.655          4.8369          6.0766
v  Pressure                 -14446      1.3952e+05           92406           74313
v  k                    4.2962e-08          2.9898        0.046824        0.073374
v  epsilon               0.0001069      4.6889e+05          794.79          38.299
v  TurbVisc             6.2363e-13         0.41838       0.002550c  Velocity[Z]                                      0.10318E+01 
c  Pressure     0.16236E+00    1297   0.28357E-01   0.51853E-01 0.57771E+00 
c  k            0.31954E+00     153   0.90948E-04   0.70466E-03 0.18162E+01 
c  epsilon      0.18718E+04      92   0.56264E-03   0.35354E+06 0.15139E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00045797                            41
a  epsilon                 -28.055                            62
a  Local Time Step      3.5881e-08                        281774


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.1365          11.454          1.3476          0.3211
v  Velocity[Y]             -9.4892          15.025          1.0819         0.76585
v  Velocity[Z]             -13.391          9.7888        -0.77355       -0.011438
v  ǁVelocityǁ             0.018501          17.655          4.8369          6.0766
v  Pressure                 -14446      1.3952e+05           92406           74313
v  k                    4.2962e-08          2.9898        0.046824        0.073374
v  epsilon               0.0001069      4.6889e+05          794.79          38.299
v  TurbVisc             6.2363e-13         0.41838       0.0025503        0.037577
v  CourantNb               0.16245       2.787e+05          295.93          66.019
v  FourierNb               0.22665      2.3653e+06           218.6          3.2405
v  total_pressure       4.8555e+05      6.3952e+05      5.9241e+05      5.7431e+05
v  Local Time Step            0.01        0.058579        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6797      2.4042e+06          514.53           69.26


 TIME FOR THE TIME STEP              514:        0.20582E+03

===============================================================


 INSTANT    0.515000000E+02   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        -0.267117102E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0       Free surface             14           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+02 0.45003E+01
   Friction velocity        uet   :  0.30966E-01 0.41299E+02
   Friction velocity        uk    :  0.30046E-01 0.41299E+02
   Dimensionless distance   yplus :  0.42023E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10865
   Nb of faces within the viscous sub-layer     :      13880
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34169E+01     580   0.22815E+00   0.38807E+01 0.31319E+01 
c  Velocity[X]                                      0.11143E+01 
c  Velocity[Y]                                      0.17659E+01 
c  Velocity[Z]                                      0.10006E+01 
c  Pressure     0.15096E+00    1196   0.25860E-01   0.47202E-01 0.40912E+00 
c  k            0.31Free surface             14           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+02 0.45003E+01
   Friction velocity        uet   :  0.30966E-01 0.41299E+02
   Friction velocity        uk    :  0.30046E-01 0.41299E+02
   Dimensionless distance   yplus :  0.42023E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10865
   Nb of faces within the viscous sub-layer     :      13880
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34169E+01     580   0.22815E+00   0.38807E+01 0.31319E+01 
c  Velocity[X]                                      0.11143E+01 
c  Velocity[Y]                                      0.17659E+01 
c  Velocity[Z]                                      0.10006E+01 
c  Pressure     0.15096E+00    1196   0.25860E-01   0.47202E-01 0.40912E+00 
c  k            0.319Free surface             14           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+02 0.45003E+01
   Friction velocity        uet   :  0.30966E-01 0.41299E+02
   Friction velocity        uk    :  0.30046E-01 0.41299E+02
   Dimensionless distance   yplus :  0.42023E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10865
   Nb of faces within the viscous sub-layer     :      13880
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34169E+01     580   0.22815E+00   0.38807E+01 0.31319E+01 
c  Velocity[X]                                      0.11143E+01 
c  Velocity[Y]                                      0.17659E+01 
c  Velocity[Z]                                      0.10006E+01 
c  Pressure     0.15096E+00    1196   0.25860E-01   0.47202E-01 0.40912E+00 
c  k            0.319Free surface             14           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+02 0.45003E+01
   Friction velocity        uet   :  0.30966E-01 0.41299E+02
   Friction velocity        uk    :  0.30046E-01 0.41299E+02
   Dimensionless distance   yplus :  0.42023E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10865
   Nb of faces within the viscous sub-layer     :      13880
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34169E+01     580   0.22815E+00   0.38807E+01 0.31319E+01 
c  Velocity[X]                                      0.11143E+01 
c  Velocity[Y]                                      0.17659E+01 
c  Velocity[Z]                                      0.10006E+01 
c  Pressure     0.15096E+00    1196   0.25860E-01   0.47202E-01 0.40912E+00 
c  k            0.31956E+00     161   0.22413E-03   0.19304E-02 0.30067E+01 
c  epsilon      0.18898E+04     102   0.96170E-03   0.57009E+06 0.19022E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0017574                             3
a  epsilon                 -61.704                             9
a  Local Time Step      3.1329e-08                        281776


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -6.077          11.632          1.3574         0.32103
v  Velocity[Y]             -9.6409          15.376          1.0621         0.76629
v  Velocity[Z]             -12.957          9.7451        -0.80423       -0.013631
v  ǁVelocityǁ             0.010362          18.038          4.8806          6.0883
v  Pressure                 -14877      1.4054e+05           93078           74710
v  k                    2.3851e-07          3.1475        0.046605        0.073342
v  epsilon               0.0023625     v  FourierNb               0.22566      2.3653e+06          218.55          3.2376
v  total_pressure       4.8482e+05      6.4103e+05      5.9338e+05      5.7489e+05
v  Local Time Step            0.01         0.07172        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6167      2.5733e+06          518.59          69.601


 TIME FOR THE TIME STEP              517:        0.20029E+03

===============================================================


 INSTANT    0.518000000E+02   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        -0.961117357E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969590E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
--------------------v  FourierNb               0.22566      2.3653e+06          218.55          3.2376
v  total_pressure       4.8482e+05      6.4103e+05      5.9338e+05      5.7489e+05
v  Local Time Step            0.01         0.07172        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6167      2.5733e+06          518.59          69.601


 TIME FOR THE TIME STEP              517:        0.19404E+03

===============================================================


 INSTANT    0.518000000E+02   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        -0.961117357E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969590E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------v  FourierNb               0.22566      2.3653e+06          218.55          3.2376
v  total_pressure       4.8482e+05      6.4103e+05      5.9338e+05      5.7489e+05
v  Local Time Step            0.01         0.07172        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6167      2.5733e+06          518.59          69.601


 TIME FOR THE TIME STEP              517:        0.19487E+03

===============================================================


 INSTANT    0.518000000E+02   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        -0.961117357E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969590E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------v  FourierNb               0.22566      2.3653e+06          218.55          3.2376
v  total_pressure       4.8482e+05      6.4103e+05      5.9338e+05      5.7489e+05
v  Local Time Step            0.01         0.07172        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6167      2.5733e+06          518.59          69.601


 TIME FOR THE TIME STEP              517:        0.19262E+03

===============================================================


 INSTANT    0.518000000E+02   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        -0.961117357E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969590E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12811E+02 0.45003E+01
   Friction velocity        uet   :  0.30797E-01 0.43256E+02
   Friction velocity        uk    :  0.30389E-01 0.43256E+02
   Dimensionless distance   yplus :  0.32291E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10934
   Nb of faces within the viscous sub-layer     :      13897
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34201E+01     592   0.22959E+00   0.37087E+01 0.30571E+01 
c  Velocity[X]                                      0.10505E+01 
c  Velocity[Y]                                      0.16165E+01 
c  Velocity[Z]                                      0.10416E+01 
c  Pressure     0.13669E+00    1228   0.22977E-01   0.41954E-01 0.39858E+00 
c  k            0.31961E+00     150   0.10013E-03   0.72936E-03 0.18480E+01 
c  epsilon      0.19719E+04      88   0.11292E-02   0.83281E+06 0.21856E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0012081                            20
a  epsilon                 -12.247                            63
a  Local Time Step      2.9298e-08                        281779


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.1307          11.767          1.3546         0.32067
v  Velocity[Y]             -9.5704          15.137          1.0627         0.76585
v  Velocity[Z]              -12.89          9.4753        -0.79203        -0.01437
v  ǁVelocityǁ             0.019794          17.431          4.8999          6.0967
v  Pressure                 -15497       1.415e+05           93688           75063
v  k                    5.8606e-08          3.6746        0.047346        0.073303
v  epsilon               0.0022781      5.3362e+05          856.92          38.738
v  TurbVisc             6.7241e-13         0.41838       0.0024731        0.037539
v  CourantNb               0.20827      3.4132e+05          300.73          66.476
v  FourierNb               0.22531      2.3653e+06          218.55          3.2358
v  total_pressure        4.845e+05       6.415e+05      5.9369e+05      5.7506e+05
v  Local Time Step            0.01        0.078892        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6451      2.4669e+06          519.28          69.711


 TIME FOR THE TIME STEP              518:        0.18995E+03

===============================================================


 INSTANT    0.519000000E+02   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        -0.201641320E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969591E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
----------------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0010456                            38
a  epsilon                 -31.854                            62
a  Local Time Step      3.2928e-08                        281777


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.9955          11.783          1.3676         0.32059
v  Velocity[Y]             -9.5365          15.106          1.0585         0.76591
v  Velocity[Z]              -12.99          9.7068        -0.79861       -0.014216
v  ǁVelocityǁ             0.014867          17.196          4.9058          6.1028
v  Pressure                 -15852      1.4189e+05           93926           75198
v  k                    2.2864e-08          3.4178        0.047274        0.073296
v  epsilon              0.00034041      5.0043e+05          850.25           38.83
v  TurbVisc             3.4941e-13         0.41837       0.0025294        0.037534
v  CourantNb               0.26034       3.037e+05          301.27           66.48
v  FourierNb               0.22507      2.3653e+06          218.72          3.2359
v  total_pressure       4.8415e+05      6.4189e+05      5.9393e+05       5.752e+05
v  Local Time Step           -----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0010456                            38
a  epsilon                 -31.854                            62
a  Local Time Step      3.2928e-08                        281777


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.9955          11.783          1.3676         0.32059
v  Velocity[Y]             -9.5365          15.106          1.0585         0.76591
v  Velocity[Z]              -12.99          9.7068        -0.79861       -0.014216
v  ǁVelocityǁ             0.014867          17.196          4.9058          6.1028
v  Pressure                 -15852      1.4189e+05           93926           75198
v  k                    2.2864e-08          3.4178        0.047274        0.073296
v  epsilon              0.00034041      5.0043e+05          850.25           38.83
v  TurbVisc             3.4941e-13         0.41837       0.0025294        0.037534
v  CourantNb               0.26034       3.037e+05          301.27           66.48
v  FourierNb               0.22507      2.3653e+06          218.72          3.2359
v  total_pressure       4.8415e+05      6.4189e+05      5.9393e+05       5.752e+05
v  Local Time Step            0.01        0.086781        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6539      2.4293e+06          519.99          69.716


 TIME FOR THE TIME STEP              519:        0.18682E+03

===============================================================


 INSTANT    0.520000000E+02   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        -0.831562885E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969591E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefi------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12925E+02 0.44999E+01
   Friction velocity        uet   :  0.25410E-01 0.53643E+02
   Friction velocity        uk    :  0.25053E-01 0.53643E+02
   Dimensionless distance   yplus :  0.59506E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11041
   Nb of faces within the viscous sub-layer     :      13710
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34284E+01     577   0.22837E+00   0.56686E+01 0.37713E+01 
c  Velocity[X]                                      0.13514E+01 
c  Velocity[Y]                                      0.33217E+01 
c  Velocity[Z]                                      0.99557E+00 
c  Pressure     0.12632E+00    1198   0.19886E-01   0.37967E-01 0.30396E+00 
c  k            0.31969E+00     152   0.10704E-03   0.85310E-03 0.19989E+01 
c  epsilon      0.20171E+04      94   0.65176E-03   0.38897E+06 0.14786E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     ---------------------------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12925E+02 0.44999E+01
   Friction velocity        uet   :  0.25410E-01 0.53643E+02
   Friction velocity        uk    :  0.25053E-01 0.53643E+02
   Dimensionless distance   yplus :  0.59506E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11041
   Nb of faces within the viscous sub-layer     :      13710
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34284E+01     577   0.22837E+00   0.56686E+01 0.37713E+01 
c  Velocity[X]                                      0.13514E+01 
c  Velocity[Y]                                      0.33217E+01 
c  Velocity[Z]                                      0.99557E+00 
c  Pressure     0.12632E+00    1198   0.19886E-01   0.37967E-01 0.30396E+00 
c  k            0.31969E+00     152   0.10704E-03   0.85310E-03 0.19989E+01 
c  epsilon      0.20171E+04      94   0.65176E-03   0.38897E+06 0.14786E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     ----------------------------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12925E+02 0.44999E+01
   Friction velocity        uet   :  0.25410E-01 0.53643E+02
   Friction velocity        uk    :  0.25053E-01 0.53643E+02
   Dimensionless distance   yplus :  0.59506E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11041
   Nb of faces within the viscous sub-layer     :      13710
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34284E+01     577   0.22837E+00   0.56686E+01 0.37713E+01 
c  Velocity[X]                                      0.13514E+01 
c  Velocity[Y]                                      0.33217E+01 
c  Velocity[Z]                                      0.99557E+00 
c  Pressure     0.12632E+00    1198   0.19886E-01   0.37967E-01 0.30396E+00 
c  k            0.31969E+00     152   0.10704E-03   0.85310E-03 0.19989E+01 
c  epsilon      0.20171E+04      94   0.65176E-03   0.38897E+06 0.14786E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     ----------------------------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12925E+02 0.44999E+01
   Friction velocity        uet   :  0.25410E-01 0.53643E+02
   Friction velocity        uk    :  0.25053E-01 0.53643E+02
   Dimensionless distance   yplus :  0.59506E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11041
   Nb of faces within the viscous sub-layer     :      13710
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34284E+01     577   0.22837E+00   0.56686E+01 0.37713E+01 
c  Velocity[X]                                      0.13514E+01 
c  Velocity[Y]                                      0.33217E+01 
c  Velocity[Z]                                      0.99557E+00 
c  Pressure     0.12632E+00    1198   0.19886E-01   0.37967E-01 0.30396E+00 
c  k            0.31969E+00     152   0.10704E-03   0.85310E-03 0.19989E+01 
c  epsilon      0.20171E+04      94   0.65176E-03   0.38897E+06 0.14786E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0010512                            28
a  epsilon                 -44.935                            54
a  Local Time Step      2.1497e-08                        281778


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.0917          11.801          1.3499         0.32104
v  Velocity[Y]              -9.657          14.753          1.0998         0.76309
v  Velocity[Z]             -14.409          8.6301        -0.81131        -0.01405
v  ǁVelocityǁ             0.015305          16.782           4.952           6.111
v  Pressure                 -16512      1.4265e+05           94455           75537
v  k                    1.8126e-07          3.4646        0.046938        0.073253
v  epsilon              0.00024068      4.7763e+05          864.17          38.965
v  TurbVisc             6.2372e-13         0.41838       0.0024226        0.037519
v  CourantNb               0.11258      4.6519e+05          304.25          66.688
v  FourierNb               0.22482      2.3653e+06           218.5          3.2322
v  total_pressure 
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5953      2.5549e+06          523.89           69.99


 TIME FOR THE TIME STEP              522:        0.18845E+03

===============================================================


 INSTANT    0.523000000E+02   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        -0.123042479E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969579E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
---------------------------------------------------------
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5953      2.5549e+06          523.89           69.99


 TIME FOR THE TIME STEP              522:        0.19295E+03

===============================================================


 INSTANT    0.523000000E+02   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        -0.123042479E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969579E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
----------------------------------------------------------
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5953      2.5549e+06          523.89           69.99


 TIME FOR THE TIME STEP              522:        0.19567E+03

===============================================================


 INSTANT    0.523000000E+02   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        -0.123042479E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969579E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
----------------------------------------------------------
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5953      2.5549e+06          523.89           69.99


 TIME FOR THE TIME STEP              522:        0.18548E+03

===============================================================


 INSTANT    0.523000000E+02   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        -0.123042479E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969579E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12774E+02 0.44998E+01
   Friction velocity        uet   :  0.31334E-01 0.46314E+02
   Friction velocity        uk    :  0.34199E-01 0.46314E+02
   Dimensionless distance   yplus :  0.55035E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11048
   Nb of faces within the viscous sub-layer     :      13691
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34272E+01     597   0.22929E+00   0.60198E+01 0.38836E+01 
c  Velocity[X]                                      0.15880E+01 
c  Velocity[Y]                                      0.34006E+01 
c  Velocity[Z]                                      0.10311E+01 
c  Pressure     0.12989E+00    1198   0.19214E-01   0.38593E-01 0.29048E+00 
c  k            0.31975E+00     145   0.65021E-04   0.56181E-03 0.16216E+01 
c  epsilon      0.20714E+04     109   0.81349E-03   0.62143E+06 0.18128E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0007593                            13
a  epsilon                 -38.655                            29
a  Local Time Step      2.3106e-08                        281777


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.9739          11.834          1.3766          0.3208
v  Velocity[Y]             -9.8334          13.931          1.0563         0.76396
v  Velocity[Z]             -14.728          10.448         -0.8005       -0.013939
v  ǁVelocityǁ             0.010011          16.762          4.9445          6.1159
v  Pressure                 -16950      1.4337e+05           95038           75957
v  k                     1.333e-07          3.7984        0.047413        0.073331
v  epsilon               0.0013817      6.8294e+05          885.48          39.088
v  TurbVisc             7.3866e-13         0.41838       0.0024331        0.037522
v  CourantNb               0.28397      4.3278e+05          304.58          66.722
v  FourierNb               0.22481      2.3653e+06          218.53          3.2323
v  total_pressure       4.8305e+05      6.4337e+05      5.9504e+05      5.7596e+05
v  Local Time Step            0.01        0.056384        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.598      2.5583e+06          523.12          69.954


 TIME FOR THE TIME STEP              523:        0.18558E+03

===============================================================


 INSTANT    0.524000000E+02   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        -0.881691140E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969576E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
---------------------------------------------a  k                   -0.00015313                            37
a  epsilon                  -1.496                            36
a  Local Time Step      2.3091e-08                        281778


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -6.068          11.869          1.3627         0.32141
v  Velocity[Y]             -9.8196          13.825          1.0552         0.76383
v  Velocity[Z]             -15.105          9.1405         -0.8207       -0.013511
v  ǁVelocityǁ            0.0063958          17.145          4.9745           6.118
v  Pressure                 -17040      1.4379e+05           95390           76240
v  k                    2.4107e-07          3.7195        0.047736         0.07336
v  epsilon               0.0009422      6.2334e+05          892.76          39.326
v  TurbVisc             5.9837e-13         0.41838       0.0024205        0.037525
v  CourantNb              0.055235      4.3308e+05          304.35           66.83
v  FourierNb               0.22483      2.3653e+06          218.51          3.2314
v  total_pressure       4.8296e+05      6.4379e+05      5.9539e+05      5.7624e+05
v  Local Time Step            0.01         0.05457        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6a  k                   -0.00015313                            37
a  epsilon                  -1.496                            36
a  Local Time Step      2.3091e-08                        281778


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -6.068          11.869          1.3627         0.32141
v  Velocity[Y]             -9.8196          13.825          1.0552         0.76383
v  Velocity[Z]             -15.105          9.1405         -0.8207       -0.013511
v  ǁVelocityǁ            0.0063958          17.145          4.9745           6.118
v  Pressure                 -17040      1.4379e+05           95390           76240
v  k                    2.4107e-07          3.7195        0.047736         0.07336
v  epsilon               0.0009422      6.2334e+05          892.76          39.326
v  TurbVisc             5.9837e-13         0.41838       0.0024205        0.037525
v  CourantNb              0.055235      4.3308e+05          304.35           66.83
v  FourierNb               0.22483      2.3653e+06          218.51          3.2314
v  total_pressure       4.8296e+05      6.4379e+05      5.9539e+05      5.7624e+05
v  Local Time Step            0.01         0.05457        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6418      2.5586e+06          522.87          70.061


 TIME FOR THE TIME STEP              524:        0.19499E+03

===============================================================


 INSTANT    0.525000000E+02   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        -0.684924500E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969589E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
----------------------------------   Dimensionless distance   yplus :  0.43720E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11164
   Nb of faces within the viscous sub-layer     :      13579
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34389E+01     583   0.24415E+00   0.55115E+01 0.37135E+01 
c  Velocity[X]                                      0.13681E+01 
c  Velocity[Y]                     Dimensionless distance   yplus :  0.43720E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11164
   Nb of faces within the viscous sub-layer     :      13579
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34389E+01     583   0.24415E+00   0.55115E+01 0.37135E+01 
c  Velocity[X]                                      0.13681E+01 
c  Velocity[Y]                      Dimensionless distance   yplus :  0.43720E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11164
   Nb of faces within the viscous sub-layer     :      13579
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34389E+01     583   0.24415E+00   0.55115E+01 0.37135E+01 
c  Velocity[X]                                      0.13681E+01 
c  Velocity[Y]                                      0.27248E+01 
c  Velocity[Z]                                      0.14186E+01 
c  Pressure     0.12160E+00    1247   0.17268E-01   0.35633E-01 0.37648E+00 
c  k            0.31987E+00     142   0.77286E-04   0.75160E-03 0.18750E+01 
c  epsilon      0.21199E+04      84   0.59781E-03   0.47447E+06 0.15557E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00099296                            10
a  epsilon                  -32.97                            28
a  Local Time Step      2.0607e-08                        281780


     Dimensionless distance   yplus :  0.43720E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11164
   Nb of faces within the viscous sub-layer     :      13579
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34389E+01     583   0.24415E+00   0.55115E+01 0.37135E+01 
c  Velocity[X]                                      0.13681E+01 
c  Velocity[Y]                                      0.27248E+01 
c  Velocity[Z]                                      0.14186E+01 
c  Pressure     0.12160E+00    1247   0.17268E-01   0.35633E-01 0.37648E+00 
c  k            0.31987E+00     142   0.77286E-04   0.75160E-03 0.18750E+01 
c  epsilon      0.21199E+04      84   0.59781E-03   0.47447E+06 0.15557E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00099296                            10
a  epsilon                  -32.97                            28
a  Local Time Step      2.0607e-08                        281780


     Dimensionless distance   yplus :  0.43720E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11164
   Nb of faces within the viscous sub-layer     :      13579
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34389E+01     583   0.24415E+00   0.55115E+01 0.37135E+01 
c  Velocity[X]                                      0.13681E+01 
c  Velocity[Y]                                      0.27248E+01 
c  Velocity[Z]                                      0.14186E+01 
c  Pressure     0.12160E+00    1247   0.17268E-01   0.35633E-01 0.37648E+00 
c  k            0.31987E+00     142   0.77286E-04   0.75160E-03 0.18750E+01 
c  epsilon      0.21199E+04      84   0.59781E-03   0.47447E+06 0.15557E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00099296                            10
a  epsilon                  -32.97                            28
a  Local Time Step      2.0607e-08                        281780


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -6.081          11.951           1.349         0.32206
v  Velocity[Y]             -9.9283          13.894          1.0971         0.76464
v  Velocity[Z]             -13.552           9.897        -0.83197       -0.013429
v  ǁVelocityǁ             0.029536          15.944          5.0065          6.1211
v  Pressure                 -17058      1.4466e+05           96136           76849
v  k                    5.0111e-08          3.8375         0.04822        0.073439
v  epsilon              0.00067933      6.5753e+05          930.91          39.529
v  TurbVisc             7.2417e-13         0.41838       0.0023976        0.037525
v  CourantNb               0.10475      4.8528e+05          310.06          67.009
v  FourierNb                0.2248      2.3653e+06           218.5          3.2315
v  total_pressure       4.8294e+05      6.4466e+05      5.9614e+05      5.7685e+05
v  Local Time Step            0.01        0.056643        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
    INSTANT    0.528000000E+02   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         0.721323135E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969581E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+0 INSTANT    0.528000000E+02   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         0.721323135E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969581E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00 INSTANT    0.528000000E+02   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         0.721323135E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969581E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12741E+02 0.46047E+01
   Friction velocity        uet   :  0.18376E-01 0.40846E+02
   Friction velocity        uk    :  0.25270E-01 0.40846E+02
   Dimensionless distance   yplus :  0.41449E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11189
   Nb of faces INSTANT    0.528000000E+02   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         0.721323135E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969581E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12741E+02 0.46047E+01
   Friction velocity        uet   :  0.18376E-01 0.40846E+02
   Friction velocity        uk    :  0.25270E-01 0.40846E+02
   Dimensionless distance   yplus :  0.41449E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11189
   Nb of faces INSTANT    0.528000000E+02   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         0.721323135E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969581E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12741E+02 0.46047E+01
   Friction velocity        uet   :  0.18376E-01 0.40846E+02
   Friction velocity        uk    :  0.25270E-01 0.40846E+02
   Dimensionless distance   yplus :  0.41449E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11189
   Nb of faces within the viscous sub-layer     :      13538
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34444E+01     603   0.23564E+00   0.61147E+01 0.39084E+01 
c  Velocity[X]                                      0.17061E+01 
c  Velocity[Y]                                      0.27293E+01 
c  Velocity[Z]                                      0.16793E+01 
c  Pressure     0.12998E+00    1225   0.17386E-01   0.37822E-01 0.31809E+00 
c  k            0.31984E+00     144   0.13238E-03   0.10660E-02 0.22327E+01 
c  epsilon      0.21275E+04     102   0.97205E-03   0.88866E+06 0.21347E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.000112                            23
a  epsilon                 -1.3871                            37
a  Local Time Step      2.3686e-08                        281778


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.9918          11.909          1.3528         0.32263
v  Velocity[Y]             -9.7933          13.896          1.0671         0.76774
v  Velocity[Z]             -15.219          9.3265        -0.83464       -0.012844
v  ǁVelocityǁ             0.011754          17.364          5.0125          6.1276
v  Pressure                 -16926      1.4547e+05           96798           77454
v  k                    6.9657e-08          3.7121        0.048305        0.073511
v  epsilon              0.00029683      6.2737e+05           926.2          39.678
v  TurbVisc              5.383e-13         0.41838        0.002409        0.037535
v  CourantNb              0.071411       4.222e+05          306.81          67.044
v  FourierNb               0.22485      2.3653e+06          218.51          3.2311
v  total_pressure       4.8307e+05      6.4547e+05       5.968e+05      5.7745e+05
v  Local Time Step            0.01        0.046981        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5859      2.5477e+06          525.32          70.275


 TIME FOR THE TIME STEP              528:        0.19893E+03

===============================================================


 INSTANT    0.529000000E+02   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         0.146501734E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969597E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12827E+02 0.44996E+01
   Friction velocity        uet   :  0.34200E-01 0.43576E+02
   Friction velocity        uk    :  0.33660E-01 0.43576E+02
   Dimensionless distance   yplus :  0.41190E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of th-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.1582          11.879          1.3348         0.32194
v  Velocity[Y]             -9.8862          13.663          1.1363         0.76724
v  Velocity[Z]             -15.514          11.057        -0.85616       -0.012815
v  ǁVelocityǁ             0.012104           17.57          5.0483          6.1336
v  Pressure                 -16923      1.4581e+05           97065           77691
v  k                    2.0043e-07           3.775        0.048769        0.073501
v  epsilon              4.4804e-05      6.4011e+05          934.16          39.824
v  TurbVisc             9.3731e-14         0.41838       0.0023993        0.037534
v  CourantNb            0.00094089      4.3521e+05          309.68          67.131
v  FourierNb               0.22491      2.3653e+06          218.51          3.2291
v  total_pressure       4.8308e+05      6.4581e+05      5.9706e+05      5.7769e+05
v  Local Time Step            0.01        0.051679        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.625      2.5607e+06           528.2           70.36


 TIME FOR THE TIME STEP              529:        0.17914E+03

===============================================================


 INSTANT    0.530000000E+02   TIME STEP NUMBER             530
 ============================================================= 




   ** BOUNDARY MASS FLOW INF-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.1582          11.879          1.3348         0.32194
v  Velocity[Y]             -9.8862          13.663          1.1363         0.76724
v  Velocity[Z]             -15.514          11.057        -0.85616       -0.012815
v  ǁVelocityǁ             0.012104           17.57          5.0483          6.1336
v  Pressure                 -16923      1.4581e+05           97065           77691
v  k                    2.0043e-07           3.775        0.048769        0.073501
v  epsilon              4.4804e-05      6.4011e+05          934.16          39.824
v  TurbVisc             9.3731e-14         0.41838       0.0023993        0.037534
v  CourantNb            0.00094089      4.3521e+05          309.68          67.131
v  FourierNb               0.22491      2.3653e+06          218.51          3.2291
v  total_pressure       4.8308e+05      6.4581e+05      5.9706e+05      5.7769e+05
v  Local Time Step            0.01        0.051679        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.625      2.5607e+06           528.2           70.36


 TIME FOR THE TIME STEP              529:        0.19484E+03

===============================================================


 INSTANT    0.530000000E+02   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        -0.955208373E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969579E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12558E+02 0.44996E+01
   Friction velocity        uet   :  0.26052E-01 0.56407E+02
   Friction velocity        uk    :  0.25863E-01 0.56407E+02
   Dimensionless distance   yplus :  0.28279E-02 0.20248E+02
   ----------------------------------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34415E+01     580   0.23888E+00   0.81522E+01 0.45045E+01 
c  Velocity[X]                                      0.20191E+01 
c  Velocity[Y]                                      0.48342E+01 
c  Velocity[Z]                                      0.12989E+01 
c  Pressure     0.12602E+00    1153   0.15821E-01   0.36271E-01 0.19731E+00 
c  k            0.31989E+00     138   0.84413E-04   0.61921E-03 0.17016E+01 
c  epsilon      0.22556E+04      89   0.86749E-03   0.91928E+06 0.20402E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00060551                            14
a  epsilon                 -42.126                            36
a  Local Time Step      1.9784e-08                        281777


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.1762          11.981          1.3511         0------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34415E+01     580   0.23888E+00   0.81522E+01 0.45045E+01 
c  Velocity[X]                                      0.20191E+01 
c  Velocity[Y]                                      0.48342E+01 
c  Velocity[Z]                                      0.12989E+01 
c  Pressure     0.12602E+00    1153   0.15821E-01   0.36271E-01 0.19731E+00 
c  k            0.31989E+00     138   0.84413E-04   0.61921E-03 0.17016E+01 
c  epsilon      0.22556E+04      89   0.86749E-03   0.91928E+06 0.20402E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00060551                            14
a  epsilon                 -42.126                            36
a  Local Time Step      1.9784e-08                        281777


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.1762          11.981          1.3511         0.------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34415E+01     580   0.23888E+00   0.81522E+01 0.45045E+01 
c  Velocity[X]                                      0.20191E+01 
c  Velocity[Y]                                      0.48342E+01 
c  Velocity[Z]                                      0.12989E+01 
c  Pressure     0.12602E+00    1153   0.15821E-01   0.36271E-01 0.19731E+00 
c  k            0.31989E+00     138   0.84413E-04   0.61921E-03 0.17016E+01 
c  epsilon      0.22556E+04      89   0.86749E-03   0.91928E+06 0.20402E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00060551                            14
a  epsilon                 -42.126                            36
a  Local Time Step      1.9784e-08                        281777


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.1762          11.981          1.3511         0.------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34415E+01     580   0.23888E+00   0.81522E+01 0.45045E+01 
c  Velocity[X]                                      0.20191E+01 
c  Velocity[Y]                                      0.48342E+01 
c  Velocity[Z]                                      0.12989E+01 
c  Pressure     0.12602E+00    1153   0.15821E-01   0.36271E-01 0.19731E+00 
c  k            0.31989E+00     138   0.84413E-04   0.61921E-03 0.17016E+01 
c  epsilon      0.22556E+04      89   0.86749E-03   0.91928E+06 0.20402E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00060551                            14
a  epsilon                 -42.126                            36
a  Local Time Step      1.9784e-08                        281777


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.1762          11.981          1.3511         0.32255
v  Velocity[Y]             -9.9108          13.581          1.0971         0.77004
v  Velocity[Z]             -13.567          10.089         -0.8343       -0.014043
v  ǁVelocityǁ            0.0097647          15.994          5.0239          6.1363
v  Pressure                 -17042      1.4642e+05           97502           78085
v  k                    8.6128e-08          3.9465        0.049425        0.073456
v  epsilon               0.0033677      6.8991e+05          988.25           39.93
v  TurbVisc             6.1048e-13         0.41838       0.0024039        0.037528
v  CourantNb              0.026689      5.0545e+05          316.18          67.239
v  FourierNb               0.22474      2.3653e+06          218.53          3.2313
v  total_pressure       4.8296e+05      6.4642e+05       5.975e+05      5.7808e+05
v  Local Time Step            0.01        0.062531        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6022       2.631e+06          534.71           70.47


 TIME FOR THE TIME STEP              531:        0.18310E+03

===============================================================


 INSTANT    0.532000000E+02   TIME STEP NUMBER             5Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.913009890E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969578E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12843E+02 0.45919E+01
   Friction velocity        uet   :  0.29825E-01 0.47534E+02
   Friction velocity        uk    :  0.31605E-01 0.47534E+02
   Dimensionless distance   yplus :  0.25649E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11282
   Nb of faces within the viscous sub-layer     :      13379
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-------------------------------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.913009890E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969578E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12843E+02 0.45919E+01
   Friction velocity        uet   :  0.29825E-01 0.47534E+02
   Friction velocity        uk    :  0.31605E-01 0.47534E+02
   Dimensionless distance   yplus :  0.25649E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11282
   Nb of faces within the viscous sub-layer     :      13379
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
--------------------------------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.913009890E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969578E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12843E+02 0.45919E+01
   Friction velocity        uet   :  0.29825E-01 0.47534E+02
   Friction velocity        uk    :  0.31605E-01 0.47534E+02
   Dimensionless distance   yplus :  0.25649E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11282
   Nb of faces within the viscous sub-layer     :      13379
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
--------------------------------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.913009890E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969578E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12843E+02 0.45919E+01
   Friction velocity        uet   :  0.29825E-01 0.47534E+02
   Friction velocity        uk    :  0.31605E-01 0.47534E+02
   Dimensionless distance   yplus :  0.25649E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11282
   Nb of faces within the viscous sub-layer     :      13379
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34428E+01     579   0.23124E+00   0.70112E+01 0.41732E+01 
c  Velocity[X]                                      0.17220E+01 
c  Velocity[Y]                                      0.40162E+01 
c  Velocity[Z]                                      0.12730E+01 
c  Pressure     0.11687E+00    1009   0.14954E-01   0.33365E-01 0.82006E-01 
c  k            0.31986E+00     148   0.10872E-03   0.70195E-03 0.18116E+01 
c  epsilon      0.21659E+04      89   0.45198E-03   0.37639E+06 0.13511E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.2989e-05                            33
a  epsilon                 -39.949                            62
a  Local Time Step      2.0852e-08                        281778


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  ---v  Velocity[Z]             -14.513           8.932        -0.85433       -0.014166
v  ǁVelocityǁ             0.015892           16.69          5.1042          6.1461
v  Pressure                 -17585      1.4676e+05           97682           78247
v  k                    2.0184e-07          3.7772        0.050174        0.073407
v  epsilon              0.00080444       6.439e+05          1002.1          40.127
v  TurbVisc             6.9405e-13         0.41838        0.002408        0.037513
v  CourantNb               0.14137      4.7694e+05          315.22          67.325
v  FourierNb                0.2242      2.3653e+06          218.54          3.2316
v  total_pressure       4.8242e+05      6.4676e+05      5.9768e+05      5.7825e+05
v  Local Time Step            0.01        0.064979        0.010001        0.010007


  ** Cv  Velocity[Z]             -14.513           8.932        -0.85433       -0.014166
v  ǁVelocityǁ             0.015892           16.69          5.1042          6.1461
v  Pressure                 -17585      1.4676e+05           97682           78247
v  k                    2.0184e-07          3.7772        0.050174        0.073407
v  epsilon              0.00080444       6.439e+05          1002.1          40.127
v  TurbVisc             6.9405e-13         0.41838        0.002408        0.037513
v  CourantNb               0.14137      4.7694e+05          315.22          67.325
v  FourierNb                0.2242      2.3653e+06          218.54          3.2316
v  total_pressure       4.8242e+05      6.4676e+05      5.9768e+05      5.7825e+05
v  Local Time Step            0.01        0.064979        0.010001        0.010007


  ** Cov  Velocity[Z]             -14.513           8.932        -0.85433       -0.014166
v  ǁVelocityǁ             0.015892           16.69          5.1042          6.1461
v  Pressure                 -17585      1.4676e+05           97682           78247
v  k                    2.0184e-07          3.7772        0.050174        0.073407
v  epsilon              0.00080444       6.439e+05          1002.1          40.127
v  TurbVisc             6.9405e-13         0.41838        0.002408        0.037513
v  CourantNb               0.14137      4.7694e+05          315.22          67.325
v  FourierNb                0.2242      2.3653e+06          218.54          3.2316
v  total_pressure       4.8242e+05      6.4676e+05      5.9768e+05      5.7825e+05
v  Local Time Step            0.01        0.064979        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6086      2.6024e+06          533.77          70.557


 TIME FOR THE TIME STEP              534:        0.17439E+03

===============================================================


 INSTANT    0.535000000E+02   TIME STEP NUMBER             535
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet         v  Velocity[Z]             -14.513           8.932        -0.85433       -0.014166
v  ǁVelocityǁ             0.015892           16.69          5.1042          6.1461
v  Pressure                 -17585      1.4676e+05           97682           78247
v  k                    2.0184e-07          3.7772        0.050174        0.073407
v  epsilon              0.00080444       6.439e+05          1002.1          40.127
v  TurbVisc             6.9405e-13         0.41838        0.002408        0.037513
v  CourantNb               0.14137      4.7694e+05          315.22          67.325
v  FourierNb                0.2242      2.3653e+06          218.54          3.2316
v  total_pressure       4.8242e+05      6.4676e+05      5.9768e+05      5.7825e+05
v  Local Time Step            0.01        0.064979        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6086      2.6024e+06          533.77          70.557


 TIME FOR THE TIME STEP              534:        0.16844E+03

===============================================================


 INSTANT    0.535000000E+02   TIME STEP NUMBER             535
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet         v  Velocity[Z]             -14.513           8.932        -0.85433       -0.014166
v  ǁVelocityǁ             0.015892           16.69          5.1042          6.1461
v  Pressure                 -17585      1.4676e+05           97682           78247
v  k                    2.0184e-07          3.7772        0.050174        0.073407
v  epsilon              0.00080444       6.439e+05          1002.1          40.127
v  TurbVisc             6.9405e-13         0.41838        0.002408        0.037513
v  CourantNb               0.14137      4.7694e+05          315.22          67.325
v  FourierNb                0.2242      2.3653e+06          218.54          3.2316
v  total_pressure       4.8242e+05      6.4676e+05      5.9768e+05      5.7825e+05
v  Local Time Step            0.01        0.064979        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6086      2.6024e+06          533.77          70.557


 TIME FOR THE TIME STEP              534:        0.17945E+03

===============================================================


 INSTANT    0.535000000E+02   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         0.533663087E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969588E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12984E+02 0.46955E+01
   Friction velocity        uet   :  0.21788E-01 0.48880E+02
   Friction velocity        uk    :  0.22308E-01 0.48880E+02
   Dimensionless distance   yplus :  0.31602E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11282
   Nb of faces within the viscous sub-layer     :      13368
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34445E+01     630   0.23826E+00   0.78364E+01 0.44112E+01 
c  Velocity[X]                                      0.18820E+01 
c  Velocity[Y]                                      0.45554E+01 
c  Velocity[Z]                                      0.13990E+01 
c  Pressure     0.10978E+00     924   0.14315E-01   0.31115E-01 0.71011E-01 
c  k            0.31995E+00     149   0.87606E-04   0.57328E-03 0.16366E+01 
c  epsilon      0.22440E+04      90   0.10330E-02   0.73657E+06 0.18303E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0015618                            17
a  epsilon                 -83.758                            45
a  Local Time Step      1.9858e-08                        281775


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -6.306          12.056          1.3495         0.32534
v  Velocity[Y]              -9.808          13.709          1.1018         0.77134
v  Velocity[Z]             -15.722          10.015        -0.84891       -0.014806
v  ǁVelocityǁ             0.020463          17.767          5.0727          6.1438
v  Pressure                 -17804      1.4684e+05           97722           78266
v  k                    1.7009e-07          3.9461        0.050005        0.073449
v  epsilon               0.0043153      7.1371e+05          1002.8          40.175
v  TurbVisc             4.8329e-13         0.41838        0.002405        0.037509
v  CourantNb              0.074041      5.0357e+05          318.64          67.481
v  FourierNb               0.22405      2.3653e+06          218.55          3.2323
v  total_pressure        4.822e+05      6.4684e+05      5.9772e+05      5.7827e+05
v  Local Time Step            0.01        0.071476        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6601      2.6291e+06          537.18          70.714


 TIME FOR THE TIME STEP              535:        0.19217E+03

===============================================================


 INSTANT    0.536000000E+02   TIME STEP NUMBER             536
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
-----------------------------------------------------------------------------
c  Velocity     0.34445E+01     579   0.23439E+00   0.69107E+01 0.41423E+01 
c  Velocity[X]                                      0.19939E+01 
c  Velocity[Y]                                      0.37196E+01 
c  Velocity[Z]                                      0.11972E+01 
c  Pressure     0.10372E+00     856   0.13227E-01   0.29331E-01 0.56436E-01 
c  k            0.31995E+00     135   0.73440E-04   0.51105E-03 0.15453E+01 
c  epsilon      0.22512E+04      91   0.72116E-03   0.64999E+06 0.17108E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0065312                            22
a  epsilon                 -283.39                            27
a  Local Time Step      1.8944e-08                        281774


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.2869          12.006          1.3632         0.32662
v  Velocity[Y]              -9.815          13.892          1.0794         0.77174
v  Velocity[Z]             -15.037           10.28        -0.83016       -0.014271
v  ǁVelocityǁ             0.022518          17.147          5.0547           6.147
v  Pressure                 ------------------------------------------------------------------------------
c  Velocity     0.34445E+01     579   0.23439E+00   0.69107E+01 0.41423E+01 
c  Velocity[X]                                      0.19939E+01 
c  Velocity[Y]                                      0.37196E+01 
c  Velocity[Z]                                      0.11972E+01 
c  Pressure     0.10372E+00     856   0.13227E-01   0.29331E-01 0.56436E-01 
c  k            0.31995E+00     135   0.73440E-04   0.51105E-03 0.15453E+01 
c  epsilon      0.22512E+04      91   0.72116E-03   0.64999E+06 0.17108E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0065312                            22
a  epsilon                 -283.39                            27
a  Local Time Step      1.8944e-08                        281774


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.2869          12.006          1.3632         0.32662
v  Velocity[Y]              -9.815          13.892          1.0794         0.77174
v  Velocity[Z]             -15.037           10.28        -0.83016       -0.014271
v  ǁVelocityǁ             0.022518          17.147          5.0547           6.147
v  Pressure                 -17969      1.4688e+05           97746           78280
v  k                    1.9837e-07           3.882        0.049885        0.073489
v  epsilon               0.0016566      6.7722e+05          996.74          40.215
v  TurbVisc             6.0136e-13         0.41838       0.0024161        0.037514
v  CourantNb              0.037985      5.2787e+05          316.13          67.332
v  FourierNb               0.22393      2.3653e+06          218.55          3.2315
v  total_pressure       4.8203e+05      6.4688e+05      5.9775e+05      5.7828e+05
v  Local Time Step            0.01        0.078624        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6077      2.6534e+06          534.68          70.563


 TIME FOR THE TIME STEP              536:        0.17666E+03

===============================================================


 INSTANT    0.537000000E+02   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         0.567011559E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969576E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12983E+02 0.45968E+01
   Friction velocity        uet   :  0.31136E-01 0.38678E+02
   Friction velocity        uk    :  0.30205E-01 0.38678E+02
   Dimensionless distance   yplus :  0.35015E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11384
   Nb of faces within the viscous sub-layer     :      13348
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      deSymmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969571E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13083E+02 0.45296E+01
   Friction velocity        uet   :  0.32919E-01 0.38284E+02
   Friction velocity        uk    :  0.32464E-01 0.38284E+02
   Dimensionless distance   yplus :  0.20332E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11354
   Nb of faces within the viscous sub-layer     :      13295
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34478E+01     586   0.23733E+00   0.77169E+01 0.43721E+01 
c  Velocity[X]                       Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969571E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13083E+02 0.45296E+01
   Friction velocity        uet   :  0.32919E-01 0.38284E+02
   Friction velocity        uk    :  0.32464E-01 0.38284E+02
   Dimensionless distance   yplus :  0.20332E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11354
   Nb of faces within the viscous sub-layer     :      13295
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34478E+01     586   0.23733E+00   0.77169E+01 0.43721E+01 
c  Velocity[X]                       Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969571E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13083E+02 0.45296E+01
   Friction velocity        uet   :  0.32919E-01 0.38284E+02
   Friction velocity        uk    :  0.32464E-01 0.38284E+02
   Dimensionless distance   yplus :  0.20332E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11354
   Nb of faces within the viscous sub-layer     :      13295
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34478E+01     586   0.23733E+00   0.77169E+01 0.43721E+01 
c  Velocity[X]                                      0.17332E+01 
c  Velocity[Y]                                      0.47913E+01 
c  Velocity[Z]                                      0.11924E+01 
c  Pressure     0.10302E+00     710   0.12540E-01   0.28918E-01 0.56395E-01 
c  k            0.31994E+00     146   0.82082E-04   0.59495E-03 0.16674E+01 
c  epsilon      0.21746E+04      95   0.57958E-03   0.41936E+06 0.14116E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0024841                            34
a  epsilon                 -55.016                            56
a  Local Time Step      2.1894e-08                        281778


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.5454          12.048          1.3492         0.32673
v  Velocity[Y]              -9.715          13.934          1.1457         0.76968
v  Velocity[Z]             -14.473           8.703        -0.86596       -0.014269
v  ǁVelocityǁ             0.016499          16.617          5.1102          6.1538
v  Pressure                 -18318        1.47e+05           97783           78303
v  k                    1.8637e-07          3.7943        0.050198        0.073491
v  epsilon               0.0043543      6.4711e+05          984.23          40.357
v  TurbVisc             1.1203e-13         0.41838       0.0024085        0.037516
v  CourantNb                0.0582      4.5676e+05          314.02          67.499
v  FourierNb               0.22413      2.3653e+06          218.52          3.2321
v  total_pressure       4.8168e+05        6.47e+05      5.9778e+05       5.783e+05
v  Local Time Step            0.01        0.053146        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6337      2.5823e+06          532.54          70.731


 TIME FOR THE TIME STEP              538:        0.17973E+03

===============================================================


 INSTANT    0.539000000E+02   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         0.222210474E-17
Rough walv  epsilon               0.0012774       6.871e+05          997.92          40.347
v  TurbVisc             5.3504e-13         0.41838       0.0024088        0.037516
v  CourantNb              0.038696      5.7608e+05          318.18          67.573
v  FourierNb               0.22412      2.3653e+06          218.54          3.2307
v  total_pressure       4.8149e+05      6.4705e+05      5.9781e+05       5.783e+05
v  Local Time Step            0.01        0.058461        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6766      2.7016e+06          536.72          70.803


 TIME FOR THE TIME STEP              539:        0.16896E+03

===============================================================


 INSTANT    0.540000000E+02   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        -0.111307061E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969589E+01
Free inlet               13 v  epsilon               0.0012774       6.871e+05          997.92          40.347
v  TurbVisc             5.3504e-13         0.41838       0.0024088        0.037516
v  CourantNb              0.038696      5.7608e+05          318.18          67.573
v  FourierNb               0.22412      2.3653e+06          218.54          3.2307
v  total_pressure       4.8149e+05      6.4705e+05      5.9781e+05       5.783e+05
v  Local Time Step            0.01        0.058461        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6766      2.7016e+06          536.72          70.803


 TIME FOR THE TIME STEP              539:        0.17252E+03

===============================================================


 INSTANT    0.540000000E+02   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        -0.111307061E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969589E+01
Free inlet               13 v  epsilon               0.0012774       6.871e+05          997.92          40.347
v  TurbVisc             5.3504e-13         0.41838       0.0024088        0.037516
v  CourantNb              0.038696      5.7608e+05          318.18          67.573
v  FourierNb               0.22412      2.3653e+06          218.54          3.2307
v  total_pressure       4.8149e+05      6.4705e+05      5.9781e+05       5.783e+05
v  Local Time Step            0.01        0.058461        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6766      2.7016e+06          536.72          70.803


 TIME FOR THE TIME STEP              539:        0.16695E+03

===============================================================


 INSTANT    0.540000000E+02   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        -0.111307061E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969589E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13057E+02 0.46517E+01
   Friction velocity        uet   :  0.30369E-01 0.45551E+02
   Friction velocity        uk    :  0.29872E-01 0.45551E+02
   Dimensionless distance   yplus :  0.27513E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11346
   Nb of faces within the viscous sub-layer     :      13243
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34487E+01     587   0.23614E+00   0.68607E+01 0.41229E+01 
c  Velocity[X]                                      0.17197E+01 
c  Velocity[Y]                                      0.40616E+01 
c  Velocity[Z]                                      0.10794E+01 
c  Pressure     0.94693E-01     909   0.11307E-01   0.26520E-01 0.67734E-01 
c  k            0.31997E+00     142   0.74037E-04   0.57079E-03 0.16332E+01 
c  epsilon      0.22602E+04      86   0.79632E-03   0.62025E+06 0.16590E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0023932                             9
a  epsilon                  -43.03                            17
a  Local Time Step      1.9763e-08                        281777


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.4309           12.07          1.3573         0.32633
v  Velocity[Y]             -9.9327          13.904           1.096           0.771
v  Velocity[Z]             -13.738          9.4599        -0.85004        -0.01448
v  ǁVelocityǁ            0.0025681          16.062          5.0793          6.1531
v  Pressure                 -18619      1.4712e+05           97852           78327
v  k                    1.9255e-07          3.9357         0.05039        0.073478
v  epsilon              0.00024562      6.8783e+05            1015          40.367
v  TurbVisc             4.9678e-13         0.41838        0.002412        0.037514
v  CourantNb               0.20612      5.0598e+05          317.75            67.5
v  FourierNb               0.22406      2.3653e+06          218.54          3.2315
v  total_pressure       4.8138e+05      6.4712e+05      5.9785e+05      5.7833e+05
v  Local Time Step            0.01        0.064307        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.604      2.6315e+06          536.29          70.731


 TIME FOR THE TIME STEP              540:        0.17326E+03

===============================================================


 INSTANT    0.541000000E+02   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        -0.695142319E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3  c  Velocity[Z]                                      0.13986E+01 
c  Pressure     0.96325E-01     685   0.11011E-01   0.26905E-01 0.53411E-01 
c  k            0.31995E+00     166   0.83369E-04   0.57453E-03 0.16384E+01 
c  epsilon      0.21906E+04      89   0.68600E-03   0.68635E+06 0.18130E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0046952                            13
a  epsilon                 -166.24                            27
a  Local Time Step      2.3718e-08                        281777


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]               -6.31          12.014          1.3533         0.32573
v  Velocity[Y]              -9.829          13.537          1.1028         0.77073
v  Velocity[Z]             -15.691          8.8537        -0.87142       -0.013975
v  ǁVelocityǁ             0.011539          17.752          5.1052          6.1553
v  Pressure                 -18752      1.4715e+05           97851           78327
v  k                    2.0389e-07          3.7854        0.050004        0.073482
v  epsilon               0.0040019      6.8653e+05          979.47          40.368
v  TurbVisc             6.1158e-13         0.41838       0.002415c  Velocity[Z]                                      0.13986E+01 
c  Pressure     0.96325E-01     685   0.11011E-01   0.26905E-01 0.53411E-01 
c  k            0.31995E+00     166   0.83369E-04   0.57453E-03 0.16384E+01 
c  epsilon      0.21906E+04      89   0.68600E-03   0.68635E+06 0.18130E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0046952                            13
a  epsilon                 -166.24                            27
a  Local Time Step      2.3718e-08                        281777


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]               -6.31          12.014          1.3533         0.32573
v  Velocity[Y]              -9.829          13.537          1.1028         0.77073
v  Velocity[Z]             -15.691          8.8537        -0.87142       -0.013975
v  ǁVelocityǁ             0.011539          17.752          5.1052          6.1553
v  Pressure                 -18752      1.4715e+05           97851           78327
v  k                    2.0389e-07          3.7854        0.050004        0.073482
v  epsilon               0.0040019      6.8653e+05          979.47          40.368
v  TurbVisc             6.1158e-13         0.41838       0.0024156        0.037515
v  CourantNb             0.0080772      4.2161e+05          314.18          67.508
v  FourierNb               0.22406      2.3653e+06          218.55          3.2319
v  total_pressure       4.8125e+05      6.4715e+05      5.9785e+05      5.7833e+05
v  Local Time Step            0.01        0.070737        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5816      2.5471e+06          532.73           70.74


 TIME FOR THE TIME STEP              541:        0.16132E+03

===============================================================


 INSTANT    0.542000000E+02   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        -0.102045595E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969881E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13013E+02 0.45453E+01
   Friction velocity        uet   :  0.17772E-01 0.49913E+02
   Friction velocity        uk    :  0.18199E-01 0.49913E+02
   Dimensionless distance   yplus :  0.42734E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11377
   Nb of faces within the viscous sub-layer     :      13189
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34500E+01     582   0.23718E+00   0.71210E+01 0.41994E+01 
c  Velocity[X]                                      0.15860E+01 
c  Velocity[Y]   Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12965E+02 0.46380E+01
   Friction velocity        uet   :  0.20074E-01 0.49907E+02
   Friction velocity        uk    :  0.20126E-01 0.49907E+02
   Dimensionless distance   yplus :  0.29978E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11424
   Nb of faces within the viscous sub-layer     :      13203
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34543E+01     567   0.23791E+00   0.61273E+01 0.38946E+01 
c  Velocity[X]                                      0.17455E+01 
c  Velocity[Y]                                      0.29469E+01 
c  Velocity[Z]                                      0.14349E+01 
c  Pressure     0.99718E-01     414   0.11267E-01   0.27818E-01 0.55288E-01 
c  k            0.320Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12965E+02 0.46380E+01
   Friction velocity        uet   :  0.20074E-01 0.49907E+02
   Friction velocity        uk    :  0.20126E-01 0.49907E+02
   Dimensionless distance   yplus :  0.29978E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11424
   Nb of faces within the viscous sub-layer     :      13203
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34543E+01     567   0.23791E+00   0.61273E+01 0.38946E+01 
c  Velocity[X]                                      0.17455E+01 
c  Velocity[Y]                                      0.29469E+01 
c  Velocity[Z]                                      0.14349E+01 
c  Pressure     0.99718E-01     414   0.11267E-01   0.27818E-01 0.55288E-01 
c  k            0.320Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12965E+02 0.46380E+01
   Friction velocity        uet   :  0.20074E-01 0.49907E+02
   Friction velocity        uk    :  0.20126E-01 0.49907E+02
   Dimensionless distance   yplus :  0.29978E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11424
   Nb of faces within the viscous sub-layer     :      13203
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34543E+01     567   0.23791E+00   0.61273E+01 0.38946E+01 
c  Velocity[X]                                      0.17455E+01 
c  Velocity[Y]                                      0.29469E+01 
c  Velocity[Z]                                      0.14349E+01 
c  Pressure     0.99718E-01     414   0.11267E-01   0.27818E-01 0.55288E-01 
c  k            0.32006E+00     134   0.10466E-03   0.70515E-03 0.18146E+01 
c  epsilon      0.22377E+04      87   0.93677E-03   0.71784E+06 0.17982E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0015989                            13
a  epsilon                 -51.635                            33
a  Local Time Step      1.8901e-08                        281774


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.3931          12.129          1.3404         0.32457
v  Velocity[Y]             -9.8966          13.763          1.1311         0.76955
v  Velocity[Z]             -15.434          9.1581        -0.87711       -0.013844
v  ǁVelocityǁ             0.018018          17.495          5.1524          6.1558
v  Pressure                 -19062      1.4717e+05           97821           78268
v  k                    4.3516e-08          3.8485         0.05093        0.073542
v  epsilon              2.9428e-05     v  FourierNb               0.22422      2.3653e+06          218.57           3.232
v  total_pressure       4.8087e+05      6.4721e+05      5.9783e+05      5.7828e+05
v  Local Time Step            0.01        0.094152        0.010001        0.010009


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6802      2.5508e+06          541.33            70.9


 TIME FOR THE TIME STEP              544:        0.16856E+03

===============================================================


 INSTANT    0.545000000E+02   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         0.716564644E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969578E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
--------------------v  FourierNb               0.22422      2.3653e+06          218.57           3.232
v  total_pressure       4.8087e+05      6.4721e+05      5.9783e+05      5.7828e+05
v  Local Time Step            0.01        0.094152        0.010001        0.010009


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6802      2.5508e+06          541.33            70.9


 TIME FOR THE TIME STEP              544:        0.17293E+03

===============================================================


 INSTANT    0.545000000E+02   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         0.716564644E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969578E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------v  FourierNb               0.22422      2.3653e+06          218.57           3.232
v  total_pressure       4.8087e+05      6.4721e+05      5.9783e+05      5.7828e+05
v  Local Time Step            0.01        0.094152        0.010001        0.010009


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6802      2.5508e+06          541.33            70.9


 TIME FOR THE TIME STEP              544:        0.17271E+03

===============================================================


 INSTANT    0.545000000E+02   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         0.716564644E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969578E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------v  FourierNb               0.22422      2.3653e+06          218.57           3.232
v  total_pressure       4.8087e+05      6.4721e+05      5.9783e+05      5.7828e+05
v  Local Time Step            0.01        0.094152        0.010001        0.010009


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6802      2.5508e+06          541.33            70.9


 TIME FOR THE TIME STEP              544:        0.16272E+03

===============================================================


 INSTANT    0.545000000E+02   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         0.716564644E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969578E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12803E+02 0.46606E+01
   Friction velocity        uet   :  0.17766E-01 0.43403E+02
   Friction velocity        uk    :  0.18342E-01 0.43403E+02
   Dimensionless distance   yplus :  0.43500E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11439
   Nb of faces within the viscous sub-layer     :      13166
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34556E+01     577   0.23909E+00   0.55932E+01 0.37217E+01 
c  Velocity[X]                                      0.18382E+01 
c  Velocity[Y]                                      0.26162E+01 
c  Velocity[Z]                                      0.11388E+01 
c  Pressure     0.91362E-01     976   0.10109E-01   0.25441E-01 0.58642E-01 
c  k            0.32015E+00     153   0.83786E-04   0.53829E-03 0.15853E+01 
c  epsilon      0.22570E+04      92   0.89631E-03   0.80458E+06 0.19177E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0029794                            22
a  epsilon                 -38.887                            23
a  Local Time Step      1.9774e-08                        281778


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.2849          12.045          1.3594         0.32375
v  Velocity[Y]             -9.8339          13.639          1.1054         0.76946
v  Velocity[Z]               -13.7           9.815        -0.86598       -0.012943
v  ǁVelocityǁ            0.0094877          16.142          5.1187          6.1564
v  Pressure                 -19200      1.4721e+05           97776           78231
v  k                     1.716e-07           3.818        0.050608        0.073658
v  epsilon               0.0039538      6.8985e+05          1009.4          40.672
v  TurbVisc             7.8294e-13         0.41838       0.0024282        0.037529
v  CourantNb              0.042143      5.0572e+05          318.34          67.556
v  FourierNb               0.22452      2.3653e+06          218.57          3.2324
v  total_pressure        4.808e+05      6.4721e+05      5.9778e+05      5.7823e+05
v  Local Time Step            0.01         0.10357        0.010001         0.01001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6637      2.6313e+06          536.91          70.789


 TIME FOR THE TIME STEP              545:        0.16899E+03

===============================================================


 INSTANT    0.546000000E+02   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         0.524800706E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969870E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
----------------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00038105                            23
a  epsilon                 -10.791                            52
a  Local Time Step      1.7611e-08                        281774


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.4371          12.133          1.3413         0.32383
v  Velocity[Y]             -9.8677          13.963          1.1378         0.76907
v  Velocity[Z]             -13.949          11.127        -0.87238       -0.012247
v  ǁVelocityǁ             0.029032          16.293          5.1492          6.1569
v  Pressure                 -19271      1.4725e+05           97754           78203
v  k                    2.3085e-07           3.774        0.050558         0.07368
v  epsilon              0.00070627      6.4425e+05          998.43          40.635
v  TurbVisc             5.4533e-13         0.41838       0.0024131        0.037536
v  CourantNb             0.0091284      5.6784e+05          317.79          67.667
v  FourierNb               0.22488      2.3653e+06          218.55          3.2325
v  total_pressure       4.8073e+05      6.4725e+05      5.9775e+05       5.782e+05
v  Local Time Step           -----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00038105                            23
a  epsilon                 -10.791                            52
a  Local Time Step      1.7611e-08                        281774


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.4371          12.133          1.3413         0.32383
v  Velocity[Y]             -9.8677          13.963          1.1378         0.76907
v  Velocity[Z]             -13.949          11.127        -0.87238       -0.012247
v  ǁVelocityǁ             0.029032          16.293          5.1492          6.1569
v  Pressure                 -19271      1.4725e+05           97754           78203
v  k                    2.3085e-07           3.774        0.050558         0.07368
v  epsilon              0.00070627      6.4425e+05          998.43          40.635
v  TurbVisc             5.4533e-13         0.41838       0.0024131        0.037536
v  CourantNb             0.0091284      5.6784e+05          317.79          67.667
v  FourierNb               0.22488      2.3653e+06          218.55          3.2325
v  total_pressure       4.8073e+05      6.4725e+05      5.9775e+05       5.782e+05
v  Local Time Step            0.01         0.11392        0.010001        0.010011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.667      2.6933e+06          536.34          70.899


 TIME FOR THE TIME STEP              546:        0.17814E+03

===============================================================


 INSTANT    0.547000000E+02   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        -0.589299061E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969906E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefi------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12760E+02 0.46821E+01
   Friction velocity        uet   :  0.10182E-01 0.33327E+02
   Friction velocity        uk    :  0.16686E-01 0.33327E+02
   Dimensionless distance   yplus :  0.37937E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11466
   Nb of faces within the viscous sub-layer     :      13148
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34580E+01     581   0.24101E+00   0.65713E+01 0.40319E+01 
c  Velocity[X]                                      0.17698E+01 
c  Velocity[Y]                                      0.34565E+01 
c  Velocity[Z]                                      0.13450E+01 
c  Pressure     0.91718E-01     927   0.10055E-01   0.25428E-01 0.59779E-01 
c  k            0.32026E+00     158   0.76939E-04   0.54184E-03 0.15898E+01 
c  epsilon      0.23378E+04      90   0.58906E-03   0.65282E+06 0.16535E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     ---------------------------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12760E+02 0.46821E+01
   Friction velocity        uet   :  0.10182E-01 0.33327E+02
   Friction velocity        uk    :  0.16686E-01 0.33327E+02
   Dimensionless distance   yplus :  0.37937E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11466
   Nb of faces within the viscous sub-layer     :      13148
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34580E+01     581   0.24101E+00   0.65713E+01 0.40319E+01 
c  Velocity[X]                                      0.17698E+01 
c  Velocity[Y]                                      0.34565E+01 
c  Velocity[Z]                                      0.13450E+01 
c  Pressure     0.91718E-01     927   0.10055E-01   0.25428E-01 0.59779E-01 
c  k            0.32026E+00     158   0.76939E-04   0.54184E-03 0.15898E+01 
c  epsilon      0.23378E+04      90   0.58906E-03   0.65282E+06 0.16535E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     ----------------------------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12760E+02 0.46821E+01
   Friction velocity        uet   :  0.10182E-01 0.33327E+02
   Friction velocity        uk    :  0.16686E-01 0.33327E+02
   Dimensionless distance   yplus :  0.37937E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11466
   Nb of faces within the viscous sub-layer     :      13148
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34580E+01     581   0.24101E+00   0.65713E+01 0.40319E+01 
c  Velocity[X]                                      0.17698E+01 
c  Velocity[Y]                                      0.34565E+01 
c  Velocity[Z]                                      0.13450E+01 
c  Pressure     0.91718E-01     927   0.10055E-01   0.25428E-01 0.59779E-01 
c  k            0.32026E+00     158   0.76939E-04   0.54184E-03 0.15898E+01 
c  epsilon      0.23378E+04      90   0.58906E-03   0.65282E+06 0.16535E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     ----------------------------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12760E+02 0.46821E+01
   Friction velocity        uet   :  0.10182E-01 0.33327E+02
   Friction velocity        uk    :  0.16686E-01 0.33327E+02
   Dimensionless distance   yplus :  0.37937E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11466
   Nb of faces within the viscous sub-layer     :      13148
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34580E+01     581   0.24101E+00   0.65713E+01 0.40319E+01 
c  Velocity[X]                                      0.17698E+01 
c  Velocity[Y]                                      0.34565E+01 
c  Velocity[Z]                                      0.13450E+01 
c  Pressure     0.91718E-01     927   0.10055E-01   0.25428E-01 0.59779E-01 
c  k            0.32026E+00     158   0.76939E-04   0.54184E-03 0.15898E+01 
c  epsilon      0.23378E+04      90   0.58906E-03   0.65282E+06 0.16535E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.002825                            20
a  epsilon                 -60.776                            24
a  Local Time Step       2.148e-08                        281776


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.5463          12.187          1.3386         0.32419
v  Velocity[Y]             -9.8045          13.856          1.1275         0.76952
v  Velocity[Z]             -14.498          8.7603         -0.8672         -0.0125
v  ǁVelocityǁ             0.026993          16.701          5.1396          6.1566
v  Pressure                 -19360      1.4741e+05           97807           78246
v  k                    9.6563e-08          3.9604        0.051553        0.073763
v  epsilon                0.003513      6.9428e+05            1065          40.978
v  TurbVisc             4.4666e-13         0.41838       0.0024186        0.037545
v  CourantNb             0.0091843      4.6556e+05          324.47           67.76
v  FourierNb               0.22525      2.3653e+06          218.57          3.2319
v  total_pressure 
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6462      2.7154e+06          540.84          70.854


 TIME FOR THE TIME STEP              549:        0.17565E+03

===============================================================


 INSTANT    0.550000000E+02   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         0.205303370E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969573E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
---------------------------------------------------------
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6462      2.7154e+06          540.84          70.854


 TIME FOR THE TIME STEP              549:        0.17168E+03

===============================================================


 INSTANT    0.550000000E+02   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         0.205303370E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969573E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
----------------------------------------------------------
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6462      2.7154e+06          540.84          70.854


 TIME FOR THE TIME STEP              549:        0.17630E+03

===============================================================


 INSTANT    0.550000000E+02   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         0.205303370E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969573E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
----------------------------------------------------------
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6462      2.7154e+06          540.84          70.854


 TIME FOR THE TIME STEP              549:        0.18218E+03

===============================================================


 INSTANT    0.550000000E+02   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         0.205303370E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969573E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12663E+02 0.45904E+01
   Friction velocity        uet   :  0.35459E-01 0.36012E+02
   Friction velocity        uk    :  0.35414E-01 0.36012E+02
   Dimensionless distance   yplus :  0.45900E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11433
   Nb of faces within the viscous sub-layer     :      13174
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34561E+01     583   0.23548E+00   0.60508E+01 0.38686E+01 
c  Velocity[X]                                      0.16655E+01 
c  Velocity[Y]                                      0.29988E+01 
c  Velocity[Z]                                      0.13865E+01 
c  Pressure     0.89348E-01     892   0.92294E-02   0.24719E-01 0.43788E-01 
c  k            0.32030E+00     144   0.93919E-04   0.71523E-03 0.18260E+01 
c  epsilon      0.22171E+04      94   0.89004E-03   0.71084E+06 0.18206E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00098741                             8
a  epsilon                 -23.456                            21
a  Local Time Step      2.1725e-08                        281778


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.3745          12.199          1.3398         0.32485
v  Velocity[Y]             -9.9052          13.984           1.124         0.77064
v  Velocity[Z]             -13.953          9.7056        -0.86786       -0.011227
v  ǁVelocityǁ            0.0099887          16.206          5.1674          6.1594
v  Pressure                 -19284      1.4754e+05           97852           78304
v  k                    3.5095e-08          3.8443        0.050718        0.073852
v  epsilon              7.9697e-05      7.1304e+05          1005.8          40.788
v  TurbVisc             6.9606e-13         0.41838        0.002428        0.037556
v  CourantNb             0.0047617      4.6029e+05          316.72          67.678
v  FourierNb               0.22531      2.3653e+06          218.58          3.2335
v  total_pressure       4.8072e+05      6.4754e+05      5.9785e+05       5.783e+05
v  Local Time Step            0.01        0.099791        0.010001         0.01001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6484      2.5858e+06           535.3          70.911


 TIME FOR THE TIME STEP              550:        0.17647E+03

===============================================================


 INSTANT    0.551000000E+02   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         0.559527961E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969567E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
---------------------------------------------a  k                   -1.5533e-05                             6
a  epsilon                -0.25194                             6
a  Local Time Step       2.505e-08                        281780


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.5433          12.215          1.3413          0.3242
v  Velocity[Y]             -9.8479          13.704          1.1647         0.77003
v  Velocity[Z]             -14.594          10.186        -0.87751       -0.011543
v  ǁVelocityǁ             0.019464          16.461           5.181          6.1637
v  Pressure                 -19258      1.4757e+05           97862           78339
v  k                    2.7905e-07          4.0592        0.052592        0.073958
v  epsilon               0.0044426      7.7288e+05          1091.8          41.369
v  TurbVisc             2.9118e-14         0.41838       0.0024275        0.037563
v  CourantNb              0.053578      3.9921e+05          322.25          67.758
v  FourierNb               0.22555      2.3653e+06          218.56          3.2333
v  total_pressure       4.8074e+05      6.4757e+05      5.9786e+05      5.7834e+05
v  Local Time Step            0.01         0.10977        0.010001         0.01001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6a  k                   -1.5533e-05                             6
a  epsilon                -0.25194                             6
a  Local Time Step       2.505e-08                        281780


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.5433          12.215          1.3413          0.3242
v  Velocity[Y]             -9.8479          13.704          1.1647         0.77003
v  Velocity[Z]             -14.594          10.186        -0.87751       -0.011543
v  ǁVelocityǁ             0.019464          16.461           5.181          6.1637
v  Pressure                 -19258      1.4757e+05           97862           78339
v  k                    2.7905e-07          4.0592        0.052592        0.073958
v  epsilon               0.0044426      7.7288e+05          1091.8          41.369
v  TurbVisc             2.9118e-14         0.41838       0.0024275        0.037563
v  CourantNb              0.053578      3.9921e+05          322.25          67.758
v  FourierNb               0.22555      2.3653e+06          218.56          3.2333
v  total_pressure       4.8074e+05      6.4757e+05      5.9786e+05      5.7834e+05
v  Local Time Step            0.01         0.10977        0.010001         0.01001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6468      2.5247e+06          540.82          70.991


 TIME FOR THE TIME STEP              551:        0.17728E+03

===============================================================


 INSTANT    0.552000000E+02   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         0.859162411E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969573E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
----------------------------------   Dimensionless distance   yplus :  0.21246E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11491
   Nb of faces within the viscous sub-layer     :      13047
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34607E+01     563   0.24238E+00   0.82439E+01 0.45131E+01 
c  Velocity[X]                                      0.20908E+01 
c  Velocity[Y]                                      0.48130E+01 
c  Velocity[Z]                                      0.13400E+01 
c  Pressure     0.89301E-01     937   0.94188E-02   0.24628E-01 0.47577E-01 
c  k            0.32060E+00     160   0.93598E-04   0.63569E-03 0.17201E+01 
c  epsilon      0.23761E+04      87   0.64815E-03   0.57860E+06 0.15265E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0023907                            17
a  epsilon                 -95.294                            23
a  Local Time Step       1.866e-08                        281774


    Dimensionless distance   yplus :  0.21246E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11491
   Nb of faces within the viscous sub-layer     :      13047
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34607E+01     563   0.24238E+00   0.82439E+01 0.45131E+01 
c  Velocity[X]                                      0.20908E+01 
c  Velocity[Y]                                      0.48130E+01 
c  Velocity[Z]                                      0.13400E+01 
c  Pressure     0.89301E-01     937   0.94188E-02   0.24628E-01 0.47577E-01 
c  k            0.32060E+00     160   0.93598E-04   0.63569E-03 0.17201E+01 
c  epsilon      0.23761E+04      87   0.64815E-03   0.57860E+06 0.15265E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0023907                            17
a  epsilon                 -95.294                            23
a  Local Time Step       1.866e-08                        281774


     Dimensionless distance   yplus :  0.21246E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11491
   Nb of faces within the viscous sub-layer     :      13047
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34607E+01     563   0.24238E+00   0.82439E+01 0.45131E+01 
c  Velocity[X]                                      0.20908E+01 
c  Velocity[Y]                                      0.48130E+01 
c  Velocity[Z]                                      0.13400E+01 
c  Pressure     0.89301E-01     937   0.94188E-02   0.24628E-01 0.47577E-01 
c  k            0.32060E+00     160   0.93598E-04   0.63569E-03 0.17201E+01 
c  epsilon      0.23761E+04      87   0.64815E-03   0.57860E+06 0.15265E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0023907                            17
a  epsilon                 -95.294                            23
a  Local Time Step       1.866e-08                        281774


     Dimensionless distance   yplus :  0.21246E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11491
   Nb of faces within the viscous sub-layer     :      13047
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34607E+01     563   0.24238E+00   0.82439E+01 0.45131E+01 
c  Velocity[X]                                      0.20908E+01 
c  Velocity[Y]                                      0.48130E+01 
c  Velocity[Z]                                      0.13400E+01 
c  Pressure     0.89301E-01     937   0.94188E-02   0.24628E-01 0.47577E-01 
c  k            0.32060E+00     160   0.93598E-04   0.63569E-03 0.17201E+01 
c  epsilon      0.23761E+04      87   0.64815E-03   0.57860E+06 0.15265E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0023907                            17
a  epsilon                 -95.294                            23
a  Local Time Step       1.866e-08                        281774


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -6.473          12.198          1.3536         0.32426
v  Velocity[Y]             -9.8156          14.355          1.1054         0.77193
v  Velocity[Z]             -15.545           8.833        -0.84697       -0.011676
v  ǁVelocityǁ             0.020079          17.641          5.1399          6.1619
v  Pressure                 -19178      1.4779e+05           97972           78432
v  k                    2.8024e-07          4.5102        0.052109        0.074051
v  epsilon               0.0006019      8.7599e+05          1091.9          41.317
v  TurbVisc             6.3619e-13         0.41838        0.002436        0.037582
v  CourantNb              0.053444      5.3592e+05          324.46          67.778
v  FourierNb               0.22638      2.3653e+06          218.59          3.2339
v  total_pressure       4.8082e+05      6.4779e+05      5.9797e+05      5.7843e+05
v  Local Time Step            0.01        0.056736        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
    INSTANT    0.555000000E+02   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        -0.854207775E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969574E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12660E+02 0.46845E+01
   Friction velocity        uet   :  0.28825E-01 0.25702E+02
   Friction velocity        uk    :  0.32001E-01 0.25702E+02
   Dimensionless distance   yplus :  0.32796E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11499
   Nb of face INSTANT    0.555000000E+02   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        -0.854207775E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969574E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12660E+02 0.46845E+01
   Friction velocity        uet   :  0.28825E-01 0.25702E+02
   Friction velocity        uk    :  0.32001E-01 0.25702E+02
   Dimensionless distance   yplus :  0.32796E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11499
   Nb of faces INSTANT    0.555000000E+02   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        -0.854207775E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969574E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12660E+02 0.46845E+01
   Friction velocity        uet   :  0.28825E-01 0.25702E+02
   Friction velocity        uk    :  0.32001E-01 0.25702E+02
   Dimensionless distance   yplus :  0.32796E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11499
   Nb of faces INSTANT    0.555000000E+02   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        -0.854207775E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969574E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12660E+02 0.46845E+01
   Friction velocity        uet   :  0.28825E-01 0.25702E+02
   Friction velocity        uk    :  0.32001E-01 0.25702E+02
   Dimensionless distance   yplus :  0.32796E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11499
   Nb of faces within the viscous sub-layer     :      12986
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34581E+01     613   0.23521E+00   0.70076E+01 0.41593E+01 
c  Velocity[X]                                      0.15980E+01 
c  Velocity[Y]                                      0.40593E+01 
c  Velocity[Z]                                      0.13502E+01 
c  Pressure     0.88343E-01     928   0.86801E-02   0.24301E-01 0.61525E-01 
c  k            0.32052E+00     143   0.10154E-03   0.63687E-03 0.17221E+01 
c  epsilon      0.22894E+04      85   0.43906E-03   0.25655E+06 0.10525E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0004597                             6
a  epsilon                 -1.0405                             7
a  Local Time Step      2.1329e-08                        281777


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.5293          12.204          1.3477         0.32402
v  Velocity[Y]             -9.7464          13.687          1.1611         0.77017
v  Velocity[Z]             -13.688           10.11        -0.88417       -0.011221
v  ǁVelocityǁ             0.019614          16.167          5.1773          6.1647
v  Pressure                 -19097      1.4793e+05           98034           78526
v  k                    2.3394e-07          4.2068        0.052283        0.074028
v  epsilon               0.0039006      7.9304e+05          1066.9          41.417
v  TurbVisc             7.8078e-13         0.41838       0.0024329        0.037588
v  CourantNb              0.043838      4.6886e+05          322.67          67.823
v  FourierNb                0.2269      2.3653e+06          218.59          3.2343
v  total_pressure        4.809e+05      6.4793e+05      5.9803e+05      5.7853e+05
v  Local Time Step            0.01         0.06865        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6325      2.5944e+06          541.25          71.057


 TIME FOR THE TIME STEP              555:        0.17705E+03

===============================================================


 INSTANT    0.556000000E+02   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         0.913546477E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969553E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12489E+02 0.46736E+01
   Friction velocity        uet   :  0.35128E-01 0.60587E+02
   Friction velocity        uk    :  0.34373E-01 0.60587E+02
   Dimensionless distance   yplus :  0.42726E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of th-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.6468          12.208           1.355         0.32403
v  Velocity[Y]             -9.7634          13.917          1.1371         0.77034
v  Velocity[Z]             -14.111          9.3811         -0.8704       -0.011711
v  ǁVelocityǁ             0.012665          16.251          5.1845          6.1642
v  Pressure                 -19077      1.4797e+05           98049           78534
v  k                    2.6579e-07          4.1139        0.052365         0.07397
v  epsilon                0.001247      7.7376e+05          1099.9          41.361
v  TurbVisc             6.9846e-13         0.41838       0.0024406        0.037583
v  CourantNb               0.14825      6.3412e+05          325.58          67.805
v  FourierNb               0.22681      2.3653e+06          218.59          3.2329
v  total_pressure       4.8092e+05      6.4797e+05      5.9805e+05      5.7853e+05
v  Local Time Step            0.01        0.075515        0.010001        0.010009


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6528      2.7596e+06          544.17          71.037


 TIME FOR THE TIME STEP              556:        0.16362E+03

===============================================================


 INSTANT    0.557000000E+02   TIME STEP NUMBER             557
 ============================================================= 




   ** BOUNDARY MASS FLOW INF-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.6468          12.208           1.355         0.32403
v  Velocity[Y]             -9.7634          13.917          1.1371         0.77034
v  Velocity[Z]             -14.111          9.3811         -0.8704       -0.011711
v  ǁVelocityǁ             0.012665          16.251          5.1845          6.1642
v  Pressure                 -19077      1.4797e+05           98049           78534
v  k                    2.6579e-07          4.1139        0.052365         0.07397
v  epsilon                0.001247      7.7376e+05          1099.9          41.361
v  TurbVisc             6.9846e-13         0.41838       0.0024406        0.037583
v  CourantNb               0.14825      6.3412e+05          325.58          67.805
v  FourierNb               0.22681      2.3653e+06          218.59          3.2329
v  total_pressure       4.8092e+05      6.4797e+05      5.9805e+05      5.7853e+05
v  Local Time Step            0.01        0.075515        0.010001        0.010009


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6528      2.7596e+06          544.17          71.037


 TIME FOR THE TIME STEP              556:        0.18066E+03

===============================================================


 INSTANT    0.557000000E+02   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        -0.626674116E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969567E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12957E+02 0.47865E+01
   Friction velocity        uet   :  0.36735E-01 0.28776E+02
   Friction velocity        uk    :  0.36855E-01 0.28776E+02
   Dimensionless distance   yplus :  0.36718E-02 0.20249E+02
   ----------------------------------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34672E+01     595   0.24309E+00   0.60462E+01 0.38636E+01 
c  Velocity[X]                                      0.17374E+01 
c  Velocity[Y]                                      0.28561E+01 
c  Velocity[Z]                                      0.14527E+01 
c  Pressure     0.87650E-01     944   0.86481E-02   0.24054E-01 0.59414E-01 
c  k            0.32056E+00     151   0.84670E-04   0.63136E-03 0.17147E+01 
c  epsilon      0.23413E+04      97   0.60879E-03   0.42787E+06 0.13404E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011137                             9
a  epsilon                 -29.355                            17
a  Local Time Step      2.5676e-08                        281778


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.5918          12.203          1.3685         0------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34672E+01     595   0.24309E+00   0.60462E+01 0.38636E+01 
c  Velocity[X]                                      0.17374E+01 
c  Velocity[Y]                                      0.28561E+01 
c  Velocity[Z]                                      0.14527E+01 
c  Pressure     0.87650E-01     944   0.86481E-02   0.24054E-01 0.59414E-01 
c  k            0.32056E+00     151   0.84670E-04   0.63136E-03 0.17147E+01 
c  epsilon      0.23413E+04      97   0.60879E-03   0.42787E+06 0.13404E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011137                             9
a  epsilon                 -29.355                            17
a  Local Time Step      2.5676e-08                        281778


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.5918          12.203          1.3685         0.------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34672E+01     595   0.24309E+00   0.60462E+01 0.38636E+01 
c  Velocity[X]                                      0.17374E+01 
c  Velocity[Y]                                      0.28561E+01 
c  Velocity[Z]                                      0.14527E+01 
c  Pressure     0.87650E-01     944   0.86481E-02   0.24054E-01 0.59414E-01 
c  k            0.32056E+00     151   0.84670E-04   0.63136E-03 0.17147E+01 
c  epsilon      0.23413E+04      97   0.60879E-03   0.42787E+06 0.13404E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011137                             9
a  epsilon                 -29.355                            17
a  Local Time Step      2.5676e-08                        281778


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.5918          12.203          1.3685         0.------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34672E+01     595   0.24309E+00   0.60462E+01 0.38636E+01 
c  Velocity[X]                                      0.17374E+01 
c  Velocity[Y]                                      0.28561E+01 
c  Velocity[Z]                                      0.14527E+01 
c  Pressure     0.87650E-01     944   0.86481E-02   0.24054E-01 0.59414E-01 
c  k            0.32056E+00     151   0.84670E-04   0.63136E-03 0.17147E+01 
c  epsilon      0.23413E+04      97   0.60879E-03   0.42787E+06 0.13404E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011137                             9
a  epsilon                 -29.355                            17
a  Local Time Step      2.5676e-08                        281778


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.5918          12.203          1.3685         0.32401
v  Velocity[Y]             -9.7689          13.819          1.1129         0.77115
v  Velocity[Z]              -14.34          9.5714        -0.87016       -0.011145
v  ǁVelocityǁ             0.021999          16.452          5.1641          6.1655
v  Pressure                 -18908      1.4809e+05           98080           78591
v  k                    3.7074e-07          4.1689        0.051928        0.073979
v  epsilon               0.0031013      7.8473e+05          1072.2          41.325
v  TurbVisc             7.5763e-13         0.41838        0.002453        0.037579
v  CourantNb               0.03292      3.8946e+05          322.56          67.737
v  FourierNb               0.22633      2.3653e+06          218.59          3.2343
v  total_pressure       4.8109e+05      6.4809e+05      5.9808e+05      5.7859e+05
v  Local Time Step            0.01        0.056463        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6529       2.515e+06          541.15          70.971


 TIME FOR THE TIME STEP              558:        0.17731E+03

===============================================================


 INSTANT    0.559000000E+02   TIME STEP NUMBER             5Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.129199746E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969545E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12942E+02 0.46413E+01
   Friction velocity        uet   :  0.25688E-01 0.53961E+02
   Friction velocity        uk    :  0.25357E-01 0.53961E+02
   Dimensionless distance   yplus :  0.42645E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11518
   Nb of faces within the viscous sub-layer     :      13079
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-------------------------------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.129199746E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969545E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12942E+02 0.46413E+01
   Friction velocity        uet   :  0.25688E-01 0.53961E+02
   Friction velocity        uk    :  0.25357E-01 0.53961E+02
   Dimensionless distance   yplus :  0.42645E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11518
   Nb of faces within the viscous sub-layer     :      13079
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
--------------------------------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.129199746E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969545E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12942E+02 0.46413E+01
   Friction velocity        uet   :  0.25688E-01 0.53961E+02
   Friction velocity        uk    :  0.25357E-01 0.53961E+02
   Dimensionless distance   yplus :  0.42645E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11518
   Nb of faces within the viscous sub-layer     :      13079
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
--------------------------------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.129199746E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969545E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12942E+02 0.46413E+01
   Friction velocity        uet   :  0.25688E-01 0.53961E+02
   Friction velocity        uk    :  0.25357E-01 0.53961E+02
   Dimensionless distance   yplus :  0.42645E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11518
   Nb of faces within the viscous sub-layer     :      13079
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34653E+01     617   0.24313E+00   0.71494E+01 0.41999E+01 
c  Velocity[X]                                      0.19564E+01 
c  Velocity[Y]                                      0.39383E+01 
c  Velocity[Z]                                      0.12547E+01 
c  Pressure     0.89305E-01     560   0.89279E-02   0.24463E-01 0.26308E-01 
c  k            0.32062E+00     142   0.91296E-04   0.67350E-03 0.17707E+01 
c  epsilon      0.22954E+04      84   0.86194E-03   0.78081E+06 0.18204E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00033658                            16
a  epsilon                 -63.089                            47
a  Local Time Step      1.7276e-08                        281776


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  ---v  Velocity[Z]             -14.937          9.6097        -0.87141       -0.011723
v  ǁVelocityǁ             0.020945          17.095           5.184          6.1651
v  Pressure                 -18705      1.4825e+05           98166           78666
v  k                    2.7795e-07          4.3021        0.052305        0.073998
v  epsilon               0.0049069       8.239e+05            1100          41.447
v  TurbVisc             5.6031e-13         0.41838       0.0024356        0.037579
v  CourantNb              0.024365      3.5748e+05          324.97           67.87
v  FourierNb               0.22643      2.3653e+06          218.58          3.2341
v  total_pressure        4.813e+05      6.4825e+05      5.9817e+05      5.7867e+05
v  Local Time Step            0.01        0.070589        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5873       2.483e+06          543.55          71.104


 TIME FOR THE TIME STEP              561:        0.17592E+03

===============================================================


 INSTANT    0.562000000E+02   TIME STEP NUMBER             562
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet        v  Velocity[Z]             -14.937          9.6097        -0.87141       -0.011723
v  ǁVelocityǁ             0.020945          17.095           5.184          6.1651
v  Pressure                 -18705      1.4825e+05           98166           78666
v  k                    2.7795e-07          4.3021        0.052305        0.073998
v  epsilon               0.0049069       8.239e+05            1100          41.447
v  TurbVisc             5.6031e-13         0.41838       0.0024356        0.037579
v  CourantNb              0.024365      3.5748e+05          324.97           67.87
v  FourierNb               0.22643      2.3653e+06          218.58          3.2341
v  total_pressure        4.813e+05      6.4825e+05      5.9817e+05      5.7867e+05
v  Local Time Step            0.01        0.070589        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5873       2.483e+06          543.55          71.104


 TIME FOR THE TIME STEP              561:        0.17241E+03

===============================================================


 INSTANT    0.562000000E+02   TIME STEP NUMBER             562
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet         v  Velocity[Z]             -14.937          9.6097        -0.87141       -0.011723
v  ǁVelocityǁ             0.020945          17.095           5.184          6.1651
v  Pressure                 -18705      1.4825e+05           98166           78666
v  k                    2.7795e-07          4.3021        0.052305        0.073998
v  epsilon               0.0049069       8.239e+05            1100          41.447
v  TurbVisc             5.6031e-13         0.41838       0.0024356        0.037579
v  CourantNb              0.024365      3.5748e+05          324.97           67.87
v  FourierNb               0.22643      2.3653e+06          218.58          3.2341
v  total_pressure        4.813e+05      6.4825e+05      5.9817e+05      5.7867e+05
v  Local Time Step            0.01        0.070589        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5873       2.483e+06          543.55          71.104


 TIME FOR THE TIME STEP              561:        0.17282E+03

===============================================================


 INSTANT    0.562000000E+02   TIME STEP NUMBER             562
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet         v  Velocity[Z]             -14.937          9.6097        -0.87141       -0.011723
v  ǁVelocityǁ             0.020945          17.095           5.184          6.1651
v  Pressure                 -18705      1.4825e+05           98166           78666
v  k                    2.7795e-07          4.3021        0.052305        0.073998
v  epsilon               0.0049069       8.239e+05            1100          41.447
v  TurbVisc             5.6031e-13         0.41838       0.0024356        0.037579
v  CourantNb              0.024365      3.5748e+05          324.97           67.87
v  FourierNb               0.22643      2.3653e+06          218.58          3.2341
v  total_pressure        4.813e+05      6.4825e+05      5.9817e+05      5.7867e+05
v  Local Time Step            0.01        0.070589        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5873       2.483e+06          543.55          71.104


 TIME FOR THE TIME STEP              561:        0.17562E+03

===============================================================


 INSTANT    0.562000000E+02   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        -0.134949233E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969552E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13216E+02 0.47286E+01
   Friction velocity        uet   :  0.26623E-01 0.21932E+02
   Friction velocity        uk    :  0.34610E-01 0.21932E+02
   Dimensionless distance   yplus :  0.23117E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11518
   Nb of faces within the viscous sub-layer     :      13022
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34650E+01     605   0.24305E+00   0.72913E+01 0.42406E+01 
c  Velocity[X]                                      0.21752E+01 
c  Velocity[Y]                                      0.38343E+01 
c  Velocity[Z]                                      0.12817E+01 
c  Pressure     0.88942E-01     871   0.87982E-02   0.24362E-01 0.27785E-01 
c  k            0.32055E+00     151   0.84608E-04   0.75173E-03 0.18711E+01 
c  epsilon      0.23615E+04      92   0.52174E-03   0.53777E+06 0.14885E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0026998                            14
a  epsilon                 -61.671                            19
a  Local Time Step      2.3123e-08                        281776


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.7087          12.193          1.3742         0.32364
v  Velocity[Y]             -9.7186          13.744          1.1134         0.77104
v  Velocity[Z]             -14.822          9.9204        -0.86038       -0.011438
v  ǁVelocityǁ             0.013017          16.947          5.1544          6.1681
v  Pressure                 -18666      1.4825e+05           98139           78659
v  k                    3.1005e-07          4.2147        0.052107        0.073976
v  epsilon               0.0052029      7.9775e+05          1077.3          41.414
v  TurbVisc             7.8371e-13         0.41838       0.0024516        0.037579
v  CourantNb                0.1945      4.3247e+05          324.27          67.812
v  FourierNb               0.22646      2.3653e+06           218.6          3.2351
v  total_pressure       4.8133e+05      6.4825e+05      5.9814e+05      5.7866e+05
v  Local Time Step            0.01        0.063235        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5907       2.558e+06          542.87          71.047


 TIME FOR THE TIME STEP              562:        0.17761E+03

===============================================================


 INSTANT    0.563000000E+02   TIME STEP NUMBER             563
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
-----------------------------------------------------------------------------
c  Velocity     0.34698E+01     572   0.24702E+00   0.64299E+01 0.39835E+01 
c  Velocity[X]                                      0.17749E+01 
c  Velocity[Y]                                      0.29357E+01 
c  Velocity[Z]                                      0.17193E+01 
c  Pressure     0.95318E-01     944   0.97247E-02   0.26079E-01 0.49940E-01 
c  k            0.32043E+00     137   0.10618E-03   0.87622E-03 0.20207E+01 
c  epsilon      0.22548E+04      88   0.10666E-02   0.89432E+06 0.20195E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.013063                            54
a  epsilon                 -1181.7                           129
a  Local Time Step      1.6578e-08                        281778


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.4955          12.148          1.3716         0.32373
v  Velocity[Y]             -9.8005          14.013          1.1078         0.77144
v  Velocity[Z]             -15.927          11.133        -0.87116       -0.011175
v  ǁVelocityǁ            0.0048034           17.97          5.1678          6.1653
v  Pressure                 ------------------------------------------------------------------------------
c  Velocity     0.34698E+01     572   0.24702E+00   0.64299E+01 0.39835E+01 
c  Velocity[X]                                      0.17749E+01 
c  Velocity[Y]                                      0.29357E+01 
c  Velocity[Z]                                      0.17193E+01 
c  Pressure     0.95318E-01     944   0.97247E-02   0.26079E-01 0.49940E-01 
c  k            0.32043E+00     137   0.10618E-03   0.87622E-03 0.20207E+01 
c  epsilon      0.22548E+04      88   0.10666E-02   0.89432E+06 0.20195E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.013063                            54
a  epsilon                 -1181.7                           129
a  Local Time Step      1.6578e-08                        281778


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.4955          12.148          1.3716         0.32373
v  Velocity[Y]             -9.8005          14.013          1.1078         0.77144
v  Velocity[Z]             -15.927          11.133        -0.87116       -0.011175
v  ǁVelocityǁ            0.0048034           17.97          5.1678          6.1653
v  Pressure                 -18660      1.4822e+05           98093           78624
v  k                     2.711e-07          4.1326        0.051159        0.073914
v  epsilon               0.0055472       7.723e+05          1015.5          41.121
v  TurbVisc             1.0234e-12         0.41838       0.0024352        0.037573
v  CourantNb             0.0099968      6.0322e+05           319.7          67.876
v  FourierNb               0.22646      2.3653e+06          218.58          3.2338
v  total_pressure       4.8134e+05      6.4822e+05      5.9809e+05      5.7862e+05
v  Local Time Step            0.01        0.069558        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5955      2.7288e+06          538.28          71.109


 TIME FOR THE TIME STEP              563:        0.17762E+03

===============================================================


 INSTANT    0.564000000E+02   TIME STEP NUMBER             564
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
----------------------------------------------Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969907E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12838E+02 0.47486E+01
   Friction velocity        uet   :  0.29616E-01 0.45764E+02
   Friction velocity        uk    :  0.29005E-01 0.45764E+02
   Dimensionless distance   yplus :  0.29169E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11555
   Nb of faces within the viscous sub-layer     :      13067
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34670E+01     590   0.23964E+00   0.76243E+01 0.43350E+01 
c  Velocity[X]                      Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969907E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12838E+02 0.47486E+01
   Friction velocity        uet   :  0.29616E-01 0.45764E+02
   Friction velocity        uk    :  0.29005E-01 0.45764E+02
   Dimensionless distance   yplus :  0.29169E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11555
   Nb of faces within the viscous sub-layer     :      13067
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34670E+01     590   0.23964E+00   0.76243E+01 0.43350E+01 
c  Velocity[X]                       Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969907E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12838E+02 0.47486E+01
   Friction velocity        uet   :  0.29616E-01 0.45764E+02
   Friction velocity        uk    :  0.29005E-01 0.45764E+02
   Dimensionless distance   yplus :  0.29169E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11555
   Nb of faces within the viscous sub-layer     :      13067
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34670E+01     590   0.23964E+00   0.76243E+01 0.43350E+01 
c  Velocity[X]                       Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969907E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12838E+02 0.47486E+01
   Friction velocity        uet   :  0.29616E-01 0.45764E+02
   Friction velocity        uk    :  0.29005E-01 0.45764E+02
   Dimensionless distance   yplus :  0.29169E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11555
   Nb of faces within the viscous sub-layer     :      13067
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34670E+01     590   0.23964E+00   0.76243E+01 0.43350E+01 
c  Velocity[X]                                      0.21441E+01 
c  Velocity[Y]                                      0.37093E+01 
c  Velocity[Z]                                      0.17709E+01 
c  Pressure     0.10290E+00     905   0.11051E-01   0.28162E-01 0.45319E-01 
c  k            0.32046E+00     147   0.10212E-03   0.80635E-03 0.19382E+01 
c  epsilon      0.23488E+04      88   0.91884E-03   0.79574E+06 0.18061E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00075847                            11
a  epsilon                 -33.095                            19
a  Local Time Step      2.7925e-08                        281777


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.4734          12.178          1.3476         0.32378
v  Velocity[Y]             -9.7537           13.84          1.1358         0.77075
v  Velocity[Z]              -15.21          8.4965        -0.88508       -0.011918
v  ǁVelocityǁ             0.018963     v  epsilon               0.0045187      8.0589e+05          1093.2          41.482
v  TurbVisc             2.4849e-14         0.41838       0.0024544        0.037563
v  CourantNb              0.073743        4.61e+05          326.26           67.91
v  FourierNb               0.22586      2.3653e+06          218.61          3.2338
v  total_pressure       4.8126e+05      6.4811e+05      5.9791e+05      5.7849e+05
v  Local Time Step            0.01        0.092582        0.010001        0.010009


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6155      2.5865e+06          544.87          71.143


 TIME FOR THE TIME STEP              566:        0.18413E+03

===============================================================


 INSTANT    0.567000000E+02   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        -0.157935631E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969873E+01
Free inlet               13v  epsilon               0.0045187      8.0589e+05          1093.2          41.482
v  TurbVisc             2.4849e-14         0.41838       0.0024544        0.037563
v  CourantNb              0.073743        4.61e+05          326.26           67.91
v  FourierNb               0.22586      2.3653e+06          218.61          3.2338
v  total_pressure       4.8126e+05      6.4811e+05      5.9791e+05      5.7849e+05
v  Local Time Step            0.01        0.092582        0.010001        0.010009


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6155      2.5865e+06          544.87          71.143


 TIME FOR THE TIME STEP              566:        0.18273E+03

===============================================================


 INSTANT    0.567000000E+02   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        -0.157935631E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969873E+01
Free inlet               13 v  epsilon               0.0045187      8.0589e+05          1093.2          41.482
v  TurbVisc             2.4849e-14         0.41838       0.0024544        0.037563
v  CourantNb              0.073743        4.61e+05          326.26           67.91
v  FourierNb               0.22586      2.3653e+06          218.61          3.2338
v  total_pressure       4.8126e+05      6.4811e+05      5.9791e+05      5.7849e+05
v  Local Time Step            0.01        0.092582        0.010001        0.010009


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6155      2.5865e+06          544.87          71.143


 TIME FOR THE TIME STEP              566:        0.17924E+03

===============================================================


 INSTANT    0.567000000E+02   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        -0.157935631E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969873E+01
Free inlet               13 v  epsilon               0.0045187      8.0589e+05          1093.2          41.482
v  TurbVisc             2.4849e-14         0.41838       0.0024544        0.037563
v  CourantNb              0.073743        4.61e+05          326.26           67.91
v  FourierNb               0.22586      2.3653e+06          218.61          3.2338
v  total_pressure       4.8126e+05      6.4811e+05      5.9791e+05      5.7849e+05
v  Local Time Step            0.01        0.092582        0.010001        0.010009


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6155      2.5865e+06          544.87          71.143


 TIME FOR THE TIME STEP              566:        0.17332E+03

===============================================================


 INSTANT    0.567000000E+02   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        -0.157935631E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969873E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12967E+02 0.46800E+01
   Friction velocity        uet   :  0.29069E-01 0.59663E+02
   Friction velocity        uk    :  0.28496E-01 0.59663E+02
   Dimensionless distance   yplus :  0.36062E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11536
   Nb of faces within the viscous sub-layer     :      13036
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34620E+01     603   0.24368E+00   0.75380E+01 0.43114E+01 
c  Velocity[X]                                      0.20764E+01 
c  Velocity[Y]                                      0.34426E+01 
c  Velocity[Z]                                      0.20191E+01 
c  Pressure     0.10606E+00     857   0.11055E-01   0.29018E-01 0.38003E-01 
c  k            0.32039E+00     148   0.10733E-03   0.10006E-02 0.21593E+01 
c  epsilon      0.22689E+04      91   0.11258E-02   0.10482E+07 0.21726E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0065612                            31
a  epsilon                 -604.23                            69
a  Local Time Step      1.5805e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.3553          12.209          1.3766           0.324
v  Velocity[Y]             -9.6971          13.997          1.1075          0.7718
v  Velocity[Z]             -15.616          9.9947        -0.86738       -0.011473
v  ǁVelocityǁ             0.014786          17.666          5.1763          6.1668
v  Pressure                 -18662       1.481e+05           97879           78474
v  k                    4.7699e-08          4.1523        0.051245        0.073941
v  epsilon              7.3048e-05       7.777e+05            1019          41.186
v  TurbVisc             1.2287e-14         0.41838       0.0024577        0.037568
v  CourantNb               0.11637      6.3271e+05          321.01          67.821
v  FourierNb               0.22568      2.3653e+06          218.62          3.2355
v  total_pressure       4.8134e+05       6.481e+05      5.9788e+05      5.7847e+05
v  Local Time Step            0.01         0.10184        0.010001        0.010009


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5946      2.7583e+06          539.63          71.056


 TIME FOR THE TIME STEP              567:        0.16570E+03

===============================================================


 INSTANT    0.568000000E+02   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        -0.232724048E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3  c  Velocity[Z]                                      0.16287E+01 
c  Pressure     0.10891E+00     919   0.11033E-01   0.29785E-01 0.38419E-01 
c  k            0.32034E+00     140   0.97886E-04   0.87375E-03 0.20176E+01 
c  epsilon      0.22652E+04      88   0.56095E-03   0.39435E+06 0.13164E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00013532                             7
a  epsilon                 -17.922                            21
a  Local Time Step      2.5257e-08                        281776


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.6398          12.238           1.357         0.32425
v  Velocity[Y]              -9.735           13.76          1.1369         0.77059
v  Velocity[Z]             -15.939          9.5541        -0.88559       -0.011666
v  ǁVelocityǁ             0.005063          17.953          5.2069          6.1715
v  Pressure                 -18606      1.4807e+05           97844           78452
v  k                    2.3528e-07          4.0634        0.051809        0.073919
v  epsilon               0.0022095      7.5474e+05          1047.5           41.29
v  TurbVisc             6.0154e-13         0.41838       0.002437c  Velocity[Z]                                      0.16287E+01 
c  Pressure     0.10891E+00     919   0.11033E-01   0.29785E-01 0.38419E-01 
c  k            0.32034E+00     140   0.97886E-04   0.87375E-03 0.20176E+01 
c  epsilon      0.22652E+04      88   0.56095E-03   0.39435E+06 0.13164E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00013532                             7
a  epsilon                 -17.922                            21
a  Local Time Step      2.5257e-08                        281776


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.6398          12.238           1.357         0.32425
v  Velocity[Y]              -9.735           13.76          1.1369         0.77059
v  Velocity[Z]             -15.939          9.5541        -0.88559       -0.011666
v  ǁVelocityǁ             0.005063          17.953          5.2069          6.1715
v  Pressure                 -18606      1.4807e+05           97844           78452
v  k                    2.3528e-07          4.0634        0.051809        0.073919
v  epsilon               0.0022095      7.5474e+05          1047.5           41.29
v  TurbVisc             6.0154e-13         0.41838       0.0024378        0.037568
v  CourantNb              0.038687      3.9593e+05          320.38          67.875
v  FourierNb               0.22562      2.3653e+06          218.57          3.2341
v  total_pressure       4.8139e+05      6.4807e+05      5.9784e+05      5.7845e+05
v  Local Time Step            0.01         0.11202        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6245      2.5214e+06          538.94          71.109


 TIME FOR THE TIME STEP              568:        0.17618E+03

===============================================================


 INSTANT    0.569000000E+02   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         0.403444018E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0       Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13202E+02 0.47446E+01
   Friction velocity        uet   :  0.26909E-01 0.34711E+02
   Friction velocity        uk    :  0.26850E-01 0.34711E+02
   Dimensionless distance   yplus :  0.43349E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11569
   Nb of faces within the viscous sub-layer     :      12983
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34633E+01     645   0.24562E+00   0.95365E+01 0.48476E+01 
c  Velocity[X]                                      0.24338E+01 
c  Velocity[Y]                                      0.52875E+01 
c  Velocity[Z]                                      0.18152E+01 
c  Pressure     0.11414E+00     970   0.11401E-01   0.31208E-01 0.49037E-01 
c  k            0.32Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13202E+02 0.47446E+01
   Friction velocity        uet   :  0.26909E-01 0.34711E+02
   Friction velocity        uk    :  0.26850E-01 0.34711E+02
   Dimensionless distance   yplus :  0.43349E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11569
   Nb of faces within the viscous sub-layer     :      12983
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34633E+01     645   0.24562E+00   0.95365E+01 0.48476E+01 
c  Velocity[X]                                      0.24338E+01 
c  Velocity[Y]                                      0.52875E+01 
c  Velocity[Z]                                      0.18152E+01 
c  Pressure     0.11414E+00     970   0.11401E-01   0.31208E-01 0.49037E-01 
c  k            0.320Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13202E+02 0.47446E+01
   Friction velocity        uet   :  0.26909E-01 0.34711E+02
   Friction velocity        uk    :  0.26850E-01 0.34711E+02
   Dimensionless distance   yplus :  0.43349E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11569
   Nb of faces within the viscous sub-layer     :      12983
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34633E+01     645   0.24562E+00   0.95365E+01 0.48476E+01 
c  Velocity[X]                                      0.24338E+01 
c  Velocity[Y]                                      0.52875E+01 
c  Velocity[Z]                                      0.18152E+01 
c  Pressure     0.11414E+00     970   0.11401E-01   0.31208E-01 0.49037E-01 
c  k            0.320Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13202E+02 0.47446E+01
   Friction velocity        uet   :  0.26909E-01 0.34711E+02
   Friction velocity        uk    :  0.26850E-01 0.34711E+02
   Dimensionless distance   yplus :  0.43349E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11569
   Nb of faces within the viscous sub-layer     :      12983
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34633E+01     645   0.24562E+00   0.95365E+01 0.48476E+01 
c  Velocity[X]                                      0.24338E+01 
c  Velocity[Y]                                      0.52875E+01 
c  Velocity[Z]                                      0.18152E+01 
c  Pressure     0.11414E+00     970   0.11401E-01   0.31208E-01 0.49037E-01 
c  k            0.32028E+00     158   0.10828E-03   0.11020E-02 0.22667E+01 
c  epsilon      0.23984E+04      88   0.12981E-02   0.11289E+07 0.21087E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00069882                            79
a  epsilon                 -23.773                           149
a  Local Time Step      1.8813e-08                        281781


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.6426          12.244          1.3744         0.32399
v  Velocity[Y]              -9.694          14.022          1.1122         0.77156
v  Velocity[Z]             -12.639          10.043        -0.86579       -0.012308
v  ǁVelocityǁ             0.011467          16.198          5.1596          6.1662
v  Pressure                 -18461      1.4815e+05           97892           78478
v  k                    1.0391e-07          4.2634        0.052731        0.073872
v  epsilon               0.0018015     v  FourierNb               0.22512      2.3653e+06          218.62          3.2357
v  total_pressure       4.8165e+05      6.4817e+05       5.979e+05       5.785e+05
v  Local Time Step            0.01        0.093087        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6165      2.7265e+06          541.56          71.043


 TIME FOR THE TIME STEP              571:        0.17434E+03

===============================================================


 INSTANT    0.572000000E+02   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        -0.625010045E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969563E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
--------------------v  FourierNb               0.22512      2.3653e+06          218.62          3.2357
v  total_pressure       4.8165e+05      6.4817e+05       5.979e+05       5.785e+05
v  Local Time Step            0.01        0.093087        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6165      2.7265e+06          541.56          71.043


 TIME FOR THE TIME STEP              571:        0.17940E+03

===============================================================


 INSTANT    0.572000000E+02   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        -0.625010045E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969563E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------v  FourierNb               0.22512      2.3653e+06          218.62          3.2357
v  total_pressure       4.8165e+05      6.4817e+05       5.979e+05       5.785e+05
v  Local Time Step            0.01        0.093087        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6165      2.7265e+06          541.56          71.043


 TIME FOR THE TIME STEP              571:        0.17235E+03

===============================================================


 INSTANT    0.572000000E+02   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        -0.625010045E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969563E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------v  FourierNb               0.22512      2.3653e+06          218.62          3.2357
v  total_pressure       4.8165e+05      6.4817e+05       5.979e+05       5.785e+05
v  Local Time Step            0.01        0.093087        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6165      2.7265e+06          541.56          71.043


 TIME FOR THE TIME STEP              571:        0.18301E+03

===============================================================


 INSTANT    0.572000000E+02   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        -0.625010045E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969563E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13277E+02 0.46175E+01
   Friction velocity        uet   :  0.33996E-01 0.47273E+02
   Friction velocity        uk    :  0.37398E-01 0.47273E+02
   Dimensionless distance   yplus :  0.53870E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11528
   Nb of faces within the viscous sub-layer     :      13081
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34599E+01     594   0.24110E+00   0.82597E+01 0.45105E+01 
c  Velocity[X]                                      0.20714E+01 
c  Velocity[Y]                                      0.43022E+01 
c  Velocity[Z]                                      0.18861E+01 
c  Pressure     0.10071E+00     464   0.98977E-02   0.27526E-01 0.31893E-01 
c  k            0.32010E+00     139   0.11046E-03   0.92003E-03 0.20719E+01 
c  epsilon      0.22718E+04      88   0.77814E-03   0.62522E+06 0.16623E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.4309e-05                             3
a  epsilon                 -8.7561                            12
a  Local Time Step       2.856e-08                        281773


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.6288           12.12          1.3597         0.32551
v  Velocity[Y]             -9.7656          13.965          1.1186         0.77162
v  Velocity[Z]             -16.013          10.392        -0.88193       -0.011472
v  ǁVelocityǁ             0.016163          18.021          5.1937          6.1691
v  Pressure                 -18320      1.4817e+05           97895           78503
v  k                    1.9165e-07          4.0417        0.051489        0.073667
v  epsilon               0.0058195      7.4787e+05          1036.2          41.094
v  TurbVisc             7.1565e-13         0.41838       0.0024353         0.03754
v  CourantNb              0.018629      3.5014e+05          319.26          67.887
v  FourierNb               0.22475      2.3653e+06          218.57          3.2333
v  total_pressure       4.8168e+05      6.4817e+05       5.979e+05       5.785e+05
v  Local Time Step            0.01          0.1024        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6176      2.4757e+06          537.82          71.121


 TIME FOR THE TIME STEP              572:        0.16070E+03

===============================================================


 INSTANT    0.573000000E+02   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         0.552119052E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969615E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
----------------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.002536                            18
a  epsilon                 -50.206                            37
a  Local Time Step      2.4259e-08                        281780


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.6914          12.133          1.3619         0.32447
v  Velocity[Y]             -9.6469           14.01          1.1527         0.77077
v  Velocity[Z]             -15.775           8.856        -0.88882       -0.011965
v  ǁVelocityǁ             0.016859           17.75          5.2231           6.171
v  Pressure                 -18372      1.4811e+05           97848           78458
v  k                    2.8428e-07          4.1578        0.053077        0.073647
v  epsilon               0.0052792      7.8241e+05          1109.6          41.447
v  TurbVisc             5.9067e-13         0.41838       0.0024406        0.037529
v  CourantNb               0.27239      4.1221e+05          324.37          67.886
v  FourierNb               0.22435      2.3653e+06          218.57          3.2332
v  total_pressure       4.8163e+05      6.4811e+05      5.9785e+05      5.7846e+05
v  Local Time Step           -----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.002536                            18
a  epsilon                 -50.206                            37
a  Local Time Step      2.4259e-08                        281780


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.6914          12.133          1.3619         0.32447
v  Velocity[Y]             -9.6469           14.01          1.1527         0.77077
v  Velocity[Z]             -15.775           8.856        -0.88882       -0.011965
v  ǁVelocityǁ             0.016859           17.75          5.2231           6.171
v  Pressure                 -18372      1.4811e+05           97848           78458
v  k                    2.8428e-07          4.1578        0.053077        0.073647
v  epsilon               0.0052792      7.8241e+05          1109.6          41.447
v  TurbVisc             5.9067e-13         0.41838       0.0024406        0.037529
v  CourantNb               0.27239      4.1221e+05          324.37          67.886
v  FourierNb               0.22435      2.3653e+06          218.57          3.2332
v  total_pressure       4.8163e+05      6.4811e+05      5.9785e+05      5.7846e+05
v  Local Time Step            0.01         0.11264        0.010001        0.010009


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6206      2.5339e+06          542.94           71.12


 TIME FOR THE TIME STEP              573:        0.18600E+03

===============================================================


 INSTANT    0.574000000E+02   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        -0.134273544E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969879E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefi------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13413E+02 0.47383E+01
   Friction velocity        uet   :  0.38160E-01 0.48084E+02
   Friction velocity        uk    :  0.39013E-01 0.48084E+02
   Dimensionless distance   yplus :  0.47461E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11537
   Nb of faces within the viscous sub-layer     :      13007
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34655E+01     603   0.24819E+00   0.93779E+01 0.48074E+01 
c  Velocity[X]                                      0.27851E+01 
c  Velocity[Y]                                      0.49187E+01 
c  Velocity[Z]                                      0.16741E+01 
c  Pressure     0.10965E+00     937   0.10655E-01   0.30057E-01 0.39290E-01 
c  k            0.32025E+00     145   0.10096E-03   0.10439E-02 0.22066E+01 
c  epsilon      0.23715E+04      88   0.92926E-03   0.60927E+06 0.15808E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     ---------------------------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13413E+02 0.47383E+01
   Friction velocity        uet   :  0.38160E-01 0.48084E+02
   Friction velocity        uk    :  0.39013E-01 0.48084E+02
   Dimensionless distance   yplus :  0.47461E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11537
   Nb of faces within the viscous sub-layer     :      13007
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34655E+01     603   0.24819E+00   0.93779E+01 0.48074E+01 
c  Velocity[X]                                      0.27851E+01 
c  Velocity[Y]                                      0.49187E+01 
c  Velocity[Z]                                      0.16741E+01 
c  Pressure     0.10965E+00     937   0.10655E-01   0.30057E-01 0.39290E-01 
c  k            0.32025E+00     145   0.10096E-03   0.10439E-02 0.22066E+01 
c  epsilon      0.23715E+04      88   0.92926E-03   0.60927E+06 0.15808E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     ----------------------------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13413E+02 0.47383E+01
   Friction velocity        uet   :  0.38160E-01 0.48084E+02
   Friction velocity        uk    :  0.39013E-01 0.48084E+02
   Dimensionless distance   yplus :  0.47461E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11537
   Nb of faces within the viscous sub-layer     :      13007
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34655E+01     603   0.24819E+00   0.93779E+01 0.48074E+01 
c  Velocity[X]                                      0.27851E+01 
c  Velocity[Y]                                      0.49187E+01 
c  Velocity[Z]                                      0.16741E+01 
c  Pressure     0.10965E+00     937   0.10655E-01   0.30057E-01 0.39290E-01 
c  k            0.32025E+00     145   0.10096E-03   0.10439E-02 0.22066E+01 
c  epsilon      0.23715E+04      88   0.92926E-03   0.60927E+06 0.15808E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     ----------------------------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13413E+02 0.47383E+01
   Friction velocity        uet   :  0.38160E-01 0.48084E+02
   Friction velocity        uk    :  0.39013E-01 0.48084E+02
   Dimensionless distance   yplus :  0.47461E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11537
   Nb of faces within the viscous sub-layer     :      13007
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34655E+01     603   0.24819E+00   0.93779E+01 0.48074E+01 
c  Velocity[X]                                      0.27851E+01 
c  Velocity[Y]                                      0.49187E+01 
c  Velocity[Z]                                      0.16741E+01 
c  Pressure     0.10965E+00     937   0.10655E-01   0.30057E-01 0.39290E-01 
c  k            0.32025E+00     145   0.10096E-03   0.10439E-02 0.22066E+01 
c  epsilon      0.23715E+04      88   0.92926E-03   0.60927E+06 0.15808E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0031307                            16
a  epsilon                 -151.18                            63
a  Local Time Step      1.8792e-08                        281778


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.4862           12.14          1.3781         0.32386
v  Velocity[Y]             -9.7616          13.618          1.0901         0.77236
v  Velocity[Z]             -14.223          10.197        -0.86075       -0.012179
v  ǁVelocityǁ            0.0090783          16.421          5.1713          6.1687
v  Pressure                 -18394      1.4809e+05           97778           78415
v  k                    1.8672e-08          4.2632        0.052093        0.073746
v  epsilon              9.8618e-05      8.0915e+05          1082.4          41.205
v  TurbVisc             1.0412e-12         0.41838       0.0024645        0.037527
v  CourantNb               0.23403      5.3215e+05          325.21          67.791
v  FourierNb                0.2241      2.3653e+06          218.61          3.2341
v  total_pressure 
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6083      2.5077e+06          539.01          71.095


 TIME FOR THE TIME STEP              576:        0.16333E+03

===============================================================


 INSTANT    0.577000000E+02   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        -0.291712627E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969575E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
---------------------------------------------------------
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6083      2.5077e+06          539.01          71.095


 TIME FOR THE TIME STEP              576:        0.16937E+03

===============================================================


 INSTANT    0.577000000E+02   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        -0.291712627E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969575E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
----------------------------------------------------------
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6083      2.5077e+06          539.01          71.095


 TIME FOR THE TIME STEP              576:        0.15342E+03

===============================================================


 INSTANT    0.577000000E+02   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        -0.291712627E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969575E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
----------------------------------------------------------
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6083      2.5077e+06          539.01          71.095


 TIME FOR THE TIME STEP              576:        0.16243E+03

===============================================================


 INSTANT    0.577000000E+02   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        -0.291712627E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969575E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13381E+02 0.46439E+01
   Friction velocity        uet   :  0.34213E-01 0.38142E+02
   Friction velocity        uk    :  0.33558E-01 0.38142E+02
   Dimensionless distance   yplus :  0.48669E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11599
   Nb of faces within the viscous sub-layer     :      12983
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34675E+01     591   0.24863E+00   0.10116E+02 0.49895E+01 
c  Velocity[X]                                      0.28669E+01 
c  Velocity[Y]                                      0.54348E+01 
c  Velocity[Z]                                      0.18140E+01 
c  Pressure     0.10917E+00     995   0.10925E-01   0.29896E-01 0.60721E-01 
c  k            0.32044E+00     153   0.15610E-03   0.13895E-02 0.25440E+01 
c  epsilon      0.23093E+04      93   0.18426E-02   0.20374E+07 0.28730E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0013099                            16
a  epsilon                 -9.3607                            12
a  Local Time Step      2.2955e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.6674           12.17            1.37         0.32285
v  Velocity[Y]             -9.6461          14.614          1.1579         0.76999
v  Velocity[Z]             -15.898          10.636        -0.89604         -0.0116
v  ǁVelocityǁ             0.012292          17.882          5.2229           6.172
v  Pressure                 -18302        1.48e+05           97715           78373
v  k                    2.8642e-07          4.1525        0.053472        0.073946
v  epsilon               0.0052545      7.7749e+05          1122.3          41.712
v  TurbVisc             6.3782e-13         0.41838       0.0024424        0.037552
v  CourantNb               0.30864      4.3563e+05          325.09          67.926
v  FourierNb               0.22472      2.3653e+06          218.59          3.2345
v  total_pressure        4.817e+05        6.48e+05      5.9772e+05      5.7837e+05
v  Local Time Step            0.01         0.10102        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5824      2.5257e+06          543.68          71.161


 TIME FOR THE TIME STEP              577:        0.18690E+03

===============================================================


 INSTANT    0.578000000E+02   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        -0.215454362E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969880E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
---------------------------------------------a  k                     -0.002595                            50
a  epsilon                 -166.63                           111
a  Local Time Step      1.6269e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.6127          12.206          1.3654         0.32336
v  Velocity[Y]             -9.7893          14.232          1.1344         0.77073
v  Velocity[Z]             -13.788           8.738        -0.87307        -0.01244
v  ǁVelocityǁ             0.012382          16.479           5.216          6.1686
v  Pressure                 -18265      1.4803e+05           97734           78383
v  k                     1.893e-07          4.0965        0.052476        0.073967
v  epsilon              0.00041284      7.6724e+05          1085.3          41.488
v  TurbVisc             1.2414e-12         0.41838       0.0024517        0.037564
v  CourantNb              0.088035      6.1465e+05          327.82           67.99
v  FourierNb               0.22516      2.3653e+06          218.62          3.2348
v  total_pressure       4.8173e+05      6.4803e+05      5.9773e+05      5.7838e+05
v  Local Time Step            0.01        0.060111        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5a  k                     -0.002595                            50
a  epsilon                 -166.63                           111
a  Local Time Step      1.6269e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.6127          12.206          1.3654         0.32336
v  Velocity[Y]             -9.7893          14.232          1.1344         0.77073
v  Velocity[Z]             -13.788           8.738        -0.87307        -0.01244
v  ǁVelocityǁ             0.012382          16.479           5.216          6.1686
v  Pressure                 -18265      1.4803e+05           97734           78383
v  k                     1.893e-07          4.0965        0.052476        0.073967
v  epsilon              0.00041284      7.6724e+05          1085.3          41.488
v  TurbVisc             1.2414e-12         0.41838       0.0024517        0.037564
v  CourantNb              0.088035      6.1465e+05          327.82           67.99
v  FourierNb               0.22516      2.3653e+06          218.62          3.2348
v  total_pressure       4.8173e+05      6.4803e+05      5.9773e+05      5.7838e+05
v  Local Time Step            0.01        0.060111        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5965      2.7402e+06          546.44          71.225


 TIME FOR THE TIME STEP              578:        0.18112E+03

===============================================================


 INSTANT    0.579000000E+02   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        -0.398278685E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969594E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
----------------------------------   Dimensionless distance   yplus :  0.37450E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11562
   Nb of faces within the viscous sub-layer     :      12977
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34600E+01     567   0.24403E+00   0.74553E+01 0.42884E+01 
c  Velocity[X]                                      0.21627E+01 
c  Velocity[Y]                                      0.34074E+01 
c  Velocity[Z]                                      0.18852E+01 
c  Pressure     0.10712E+00     957   0.10688E-01   0.29371E-01 0.45271E-01 
c  k            0.32031E+00     133   0.10447E-03   0.10672E-02 0.22307E+01 
c  epsilon      0.23372E+04      86   0.92194E-03   0.95559E+06 0.20130E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0067733                            10
a  epsilon                 -97.335                            17
a  Local Time Step        2.44e-08                        281780


    Dimensionless distance   yplus :  0.37450E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11562
   Nb of faces within the viscous sub-layer     :      12977
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34600E+01     567   0.24403E+00   0.74553E+01 0.42884E+01 
c  Velocity[X]                                      0.21627E+01 
c  Velocity[Y]                                      0.34074E+01 
c  Velocity[Z]                                      0.18852E+01 
c  Pressure     0.10712E+00     957   0.10688E-01   0.29371E-01 0.45271E-01 
c  k            0.32031E+00     133   0.10447E-03   0.10672E-02 0.22307E+01 
c  epsilon      0.23372E+04      86   0.92194E-03   0.95559E+06 0.20130E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0067733                            10
a  epsilon                 -97.335                            17
a  Local Time Step        2.44e-08                        281780


     Dimensionless distance   yplus :  0.37450E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11562
   Nb of faces within the viscous sub-layer     :      12977
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34600E+01     567   0.24403E+00   0.74553E+01 0.42884E+01 
c  Velocity[X]                                      0.21627E+01 
c  Velocity[Y]                                      0.34074E+01 
c  Velocity[Z]                                      0.18852E+01 
c  Pressure     0.10712E+00     957   0.10688E-01   0.29371E-01 0.45271E-01 
c  k            0.32031E+00     133   0.10447E-03   0.10672E-02 0.22307E+01 
c  epsilon      0.23372E+04      86   0.92194E-03   0.95559E+06 0.20130E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0067733                            10
a  epsilon                 -97.335                            17
a  Local Time Step        2.44e-08                        281780


     Dimensionless distance   yplus :  0.37450E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11562
   Nb of faces within the viscous sub-layer     :      12977
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34600E+01     567   0.24403E+00   0.74553E+01 0.42884E+01 
c  Velocity[X]                                      0.21627E+01 
c  Velocity[Y]                                      0.34074E+01 
c  Velocity[Z]                                      0.18852E+01 
c  Pressure     0.10712E+00     957   0.10688E-01   0.29371E-01 0.45271E-01 
c  k            0.32031E+00     133   0.10447E-03   0.10672E-02 0.22307E+01 
c  epsilon      0.23372E+04      86   0.92194E-03   0.95559E+06 0.20130E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0067733                            10
a  epsilon                 -97.335                            17
a  Local Time Step        2.44e-08                        281780


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.5352          12.025          1.3635         0.32515
v  Velocity[Y]              -9.748          13.694          1.1148         0.77168
v  Velocity[Z]             -15.516           10.31        -0.88306       -0.012072
v  ǁVelocityǁ             0.016915          17.523           5.194          6.1666
v  Pressure                 -18038      1.4818e+05           97860           78496
v  k                    2.5463e-07          4.0777         0.05206        0.073899
v  epsilon               0.0054579      7.5931e+05          1064.9          41.356
v  TurbVisc             7.6433e-13         0.41838       0.0024678         0.03757
v  CourantNb               0.12794      4.0984e+05          321.68           67.86
v  FourierNb               0.22548      2.3653e+06          218.62          3.2357
v  total_pressure       4.8196e+05      6.4818e+05      5.9786e+05       5.785e+05
v  Local Time Step            0.01        0.072734        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
    INSTANT    0.582000000E+02   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         0.645168630E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969875E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13175E+02 0.46346E+01
   Friction velocity        uet   :  0.32607E-01 0.57879E+02
   Friction velocity        uk    :  0.33505E-01 0.57879E+02
   Dimensionless distance   yplus :  0.37399E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11597
   Nb of faces within the viscous sub-layer     :      12998
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34641E+01     618   0.24520E+00   0.81608E+01 0.44831E+01 
c  Velocity[X]                                      0.24500E+01 
c  Velocity[Y]                                      0.39379E+01 
c  Velocity[Z]                                      0.17729E+01 
c  Pressure     0.10486E+00     904   0.10407E-01   0.28733E-01 0.39426E-01 
c  k            0.32024E+00     146   0.12101E-03   0.97489E-03 0.21321E+01 
c  epsilon      0.23350E+04      86   0.79541E-03   0.70798E+06 0.17128E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0015741                            35
a  epsilon                 -41.958                            98
a  Local Time Step      1.5758e-08                        281775


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  INSTANT    0.582000000E+02   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         0.645168630E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969875E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13175E+02 0.46346E+01
   Friction velocity        uet   :  0.32607E-01 0.57879E+02
   Friction velocity        uk    :  0.33505E-01 0.57879E+02
   Dimensionless distance   yplus :  0.37399E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11597
   Nb of faces INSTANT    0.582000000E+02   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         0.645168630E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969875E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13175E+02 0.46346E+01
   Friction velocity        uet   :  0.32607E-01 0.57879E+02
   Friction velocity        uk    :  0.33505E-01 0.57879E+02
   Dimensionless distance   yplus :  0.37399E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11597
   Nb of faces within the viscous sub-layer     :      12998
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34641E+01     618   0.24520E+00   0.81608E+01 0.44831E+01 
c  Velocity[X]                                      0.24500E+01 
c  Velocity[Y]                                      0.39379E+01 
c  Velocity[Z]                                      0.17729E+01 
c  Pressure     0.10486E+00     904   0.10407E-01   0.28733E-01 0.39426E-01 
c  k            0.32024E+00     146   0.12101E-03   0.97489E-03 0.21321E+01 
c  epsilon      0.23350E+04      86   0.79541E-03   0.70798E+06 0.17128E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0015741                            35
a  epsilon                 -41.958                            98
a  Local Time Step      1.5758e-08                        281775


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.8391          11.991          1.3595         0.32356
v  Velocity[Y]              -9.851           14.28          1.1342         0.77201
v  Velocity[Z]             -14.257          10.123        -0.87434       -0.012894
v  ǁVelocityǁ             0.022446          16.531          5.2177          6.1707
v  Pressure                 -18138      1.4809e+05           97765           78417
v  k                     1.606e-07          4.0697         0.05292        0.073772
v  epsilon              2.0139e-05      7.6066e+05          1096.6          41.402
v  TurbVisc             1.3718e-12         0.41838       0.0024609        0.037546
v  CourantNb              0.087995      6.3458e+05          327.46          67.948
v  FourierNb               0.22499      2.3653e+06          218.63          3.2352
v  total_pressure       4.8186e+05      6.4809e+05      5.9777e+05      5.7842e+05
v  Local Time Step            0.01        0.088008        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5849      2.7602e+06          546.09          71.183


 TIME FOR THE TIME STEP              582:        0.19164E+03

===============================================================


 INSTANT    0.583000000E+02   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        -0.903643906E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969871E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13101E+02 0.47810E+01
   Friction velocity        uet   :  0.33769E-01 0.44793E+02
   Friction velocity        uk    :  0.33312E-01 0.44793E+02
   Dimensionless distance   yplus :  0.36848E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of th-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.4685           11.96          1.3553         0.32393
v  Velocity[Y]             -9.7955          13.999           1.105         0.77291
v  Velocity[Z]             -15.573          8.4751        -0.87837       -0.013144
v  ǁVelocityǁ             0.006194          17.615          5.1806          6.1679
v  Pressure                 -18211      1.4806e+05           97707           78383
v  k                    1.0513e-07          4.3685        0.053188        0.073818
v  epsilon              0.00060699      8.4207e+05          1126.4          41.431
v  TurbVisc             9.2298e-13         0.41838       0.0024594         0.03754
v  CourantNb               0.14739      3.6119e+05          326.63          67.954
v  FourierNb               0.22468      2.3653e+06          218.63          3.2342
v  total_pressure       4.8179e+05      6.4806e+05      5.9771e+05      5.7838e+05
v  Local Time Step            0.01        0.096809        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6028      2.4877e+06          545.26          71.188


 TIME FOR THE TIME STEP              583:        0.19387E+03

===============================================================


 INSTANT    0.584000000E+02   TIME STEP NUMBER             584
 ============================================================= 




   ** BOUNDARY MASS FLOW INF-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.4685           11.96          1.3553         0.32393
v  Velocity[Y]             -9.7955          13.999           1.105         0.77291
v  Velocity[Z]             -15.573          8.4751        -0.87837       -0.013144
v  ǁVelocityǁ             0.006194          17.615          5.1806          6.1679
v  Pressure                 -18211      1.4806e+05           97707           78383
v  k                    1.0513e-07          4.3685        0.053188        0.073818
v  epsilon              0.00060699      8.4207e+05          1126.4          41.431
v  TurbVisc             9.2298e-13         0.41838       0.0024594         0.03754
v  CourantNb               0.14739      3.6119e+05          326.63          67.954
v  FourierNb               0.22468      2.3653e+06          218.63          3.2342
v  total_pressure       4.8179e+05      6.4806e+05      5.9771e+05      5.7838e+05
v  Local Time Step            0.01        0.096809        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6028      2.4877e+06          545.26          71.188


 TIME FOR THE TIME STEP              583:        0.18813E+03

===============================================================


 INSTANT    0.584000000E+02   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        -0.112778445E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969877E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           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+02 0.47008E+01
   Friction velocity        uet   :  0.32736E-01 0.46869E+02
   Friction velocity        uk    :  0.34102E-01 0.46869E+02
   Dimensionless distance   yplus :  0.47451E-02 0.20249E+02
   ----------------------------------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34589E+01     621   0.24808E+00   0.75969E+01 0.43254E+01 
c  Velocity[X]                                      0.21419E+01 
c  Velocity[Y]                                      0.37176E+01 
c  Velocity[Z]                                      0.17374E+01 
c  Pressure     0.10871E+00     920   0.10892E-01   0.29848E-01 0.36904E-01 
c  k            0.32031E+00     162   0.92826E-04   0.90373E-03 0.20519E+01 
c  epsilon      0.22989E+04      91   0.62224E-03   0.40039E+06 0.13141E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00067347                            54
a  epsilon                 -9.2485                           114
a  Local Time Step      1.9715e-08                        281780


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.5678          12.094          1.3674         0.32354
v  Velocity[Y]             -9.7953          14.071          1.1367         0.77211
v  Velocity[Z]             -15.736          10.041        -0.89293        -0.01215
v  ǁVelocityǁ             0.012374          17.769          5.2053          6.1697
v  Pressure                 -18255      1.4795e+05           97593           78316
v  k                    1.0952e-07          4.1017        0.052866        0.073964
v  epsilon               0.0028535      7.6395e+05          1074.2          41.485
v  TurbVisc             1.0902e-12         0.41838       0.0024604        0.037554
v  CourantNb                0.2412      5.0723e+05          323.09          67.893
v  FourierNb               0.22462      2.3653e+06          218.64          3.2346
v  total_pressure       4.8175e+05      6.4795e+05      5.9759e+05      5.7832e+05
v  Local Time Step            0.01        0.052291        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5892      2.6328e+06          541.73          71.128


 TIME FOR THE TIME STEP              585:        0.19930E+03

===============================================================


 INSTANT    0.586000000E+02   TIME STEP NUMBER             586
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces         ------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34589E+01     621   0.24808E+00   0.75969E+01 0.43254E+01 
c  Velocity[X]                                      0.21419E+01 
c  Velocity[Y]                                      0.37176E+01 
c  Velocity[Z]                                      0.17374E+01 
c  Pressure     0.10871E+00     920   0.10892E-01   0.29848E-01 0.36904E-01 
c  k            0.32031E+00     162   0.92826E-04   0.90373E-03 0.20519E+01 
c  epsilon      0.22989E+04      91   0.62224E-03   0.40039E+06 0.13141E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00067347                            54
a  epsilon                 -9.2485                           114
a  Local Time Step      1.9715e-08                        281780


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.5678          12.094          1.3674         0.------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34589E+01     621   0.24808E+00   0.75969E+01 0.43254E+01 
c  Velocity[X]                                      0.21419E+01 
c  Velocity[Y]                                      0.37176E+01 
c  Velocity[Z]                                      0.17374E+01 
c  Pressure     0.10871E+00     920   0.10892E-01   0.29848E-01 0.36904E-01 
c  k            0.32031E+00     162   0.92826E-04   0.90373E-03 0.20519E+01 
c  epsilon      0.22989E+04      91   0.62224E-03   0.40039E+06 0.13141E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00067347                            54
a  epsilon                 -9.2485                           114
a  Local Time Step      1.9715e-08                        281780


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.5678          12.094          1.3674         0.32354
v  Velocity[Y]             -9.7953          14.071          1.1367         0.77211
v  Velocity[Z]             -15.736          10.041        -0.89293        -0.01215
v  ǁVelocityǁ             0.012374          17.769          5.2053          6.1697
v  Pressure                 -18255      1.4795e+05           97593           78316
v  k                    1.0952e-07          4.1017        0.052866        0.073964
v  epsilon               0.0028535      7.6395e+05          1074.2          41.485
v  TurbVisc             1.0902e-12         0.41838       0.0024604        0.037554
v  CourantNb                0.2412      5.0723e+05          323.09          67.893
v  FourierNb               0.22462      2.3653e+06          218.64          3.2346
v  total_pressure       4.8175e+05      6.4795e+05      5.9759e+05      5.7832e+05
v  Local Time Step            0.01        0.052291        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5892      2.6328e+06          541.73          71.128


 TIME FOR THE TIME STEP              585:        0.18844E+03

===============================================================


 INSTANT    0.586000000E+02   TIME STEP NUMBER             5Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.451578309E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969565E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13268E+02 0.47426E+01
   Friction velocity        uet   :  0.34011E-01 0.56662E+02
   Friction velocity        uk    :  0.33593E-01 0.56662E+02
   Dimensionless distance   yplus :  0.42972E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11569
   Nb of faces within the viscous sub-layer     :      12969
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34584E+01     590   0.24413E+00   0.82690E+01 0.45131E+01 
c  Velocity[X]                                      0.21256E+01 
c  Velocity[Y]                                      0.42362E+01 
c  Velocity[Z]                                      0.19073E+01 
c  Pressure     0.11271E+00    1027   0.11204E-01   0.30930E-01 0.80592E-01 
c  k            0.32037E+00     148   0.96955E-04   0.89414E-03 0.20406E+01 
c  epsilon      0.24025E+04      90   0.82447E-03   0.51742E+06 0.14276E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0010471                             6
a  epsilon                 -7.3896                            17
a  Local Time Step      2.7364e-08                        281780


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.5213          12.192          1.3527         0.32458
v  Velocity[Y]             -9.7125           13.93           1.104         0.77182
v  Velocity[Z]             -16.005          10.555        -0.88363      Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.451578309E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969565E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13268E+02 0.47426E+01
   Friction velocity        uet   :  0.34011E-01 0.56662E+02
   Friction velocity        uk    :  0.33593E-01 0.56662E+02
   Dimensionless distance   yplus :  0.42972E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11569
   Nb of faces within the viscous sub-layer     :      12969
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
--------------------------------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.451578309E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969565E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13268E+02 0.47426E+01
   Friction velocity        uet   :  0.34011E-01 0.56662E+02
   Friction velocity        uk    :  0.33593E-01 0.56662E+02
   Dimensionless distance   yplus :  0.42972E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11569
   Nb of faces within the viscous sub-layer     :      12969
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34584E+01     590   0.24413E+00   0.82690E+01 0.45131E+01 
c  Velocity[X]                                      0.21256E+01 
c  Velocity[Y]                                      0.42362E+01 
c  Velocity[Z]                                      0.19073E+01 
c  Pressure     0.11271E+00    1027   0.11204E-01   0.30930E-01 0.80592E-01 
c  k            0.32037E+00     148   0.96955E-04   0.89414E-03 0.20406E+01 
c  epsilon      0.24025E+04      90   0.82447E-03   0.51742E+06 0.14276E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0010471                             6
a  epsilon                 -7.3896                            17
a  Local Time Step      2.7364e-08                        281780


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  ---v  Velocity[Z]             -12.581           8.626        -0.87764       -0.012342
v  ǁVelocityǁ             0.021032          16.286           5.181          6.1706
v  Pressure                 -18043      1.4812e+05           97723           78435
v  k                    2.9987e-07          4.1548        0.053097         0.07403
v  epsilon               0.0056927      7.7986e+05            1099          41.652
v  TurbVisc             5.6387e-13         0.41838       0.0024883        0.037579
v  CourantNb               0.15799       4.556e+05          325.48           67.86
v  FourierNb               0.22518      2.3653e+06          218.65          3.2376
v  total_pressure       4.8196e+05      6.4812e+05      5.9772e+05      5.7844e+05
v  Local Time Step            0.01        0.069599        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6069      2.5046e+06          544.13          71.098


 TIME FOR THE TIME STEP              588:        0.18978E+03

===============================================================


 INSTANT    0.589000000E+02   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         0.938261216E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969553E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13414E+02 0.46292E+01
   Friction velocity        uet   :  0.34309E-01 0.33867E+02
   Friction velocity        uk    :  0.33599E-01 0.33867E+02
   Dimensionless distance   yplus :  0.37044E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11592
   Nb of faces within the viscous sub-layer     :      13006
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-------------v  Velocity[Z]             -12.581           8.626        -0.87764       -0.012342
v  ǁVelocityǁ             0.021032          16.286           5.181          6.1706
v  Pressure                 -18043      1.4812e+05           97723           78435
v  k                    2.9987e-07          4.1548        0.053097         0.07403
v  epsilon               0.0056927      7.7986e+05            1099          41.652
v  TurbVisc             5.6387e-13         0.41838       0.0024883        0.037579
v  CourantNb               0.15799       4.556e+05          325.48           67.86
v  FourierNb               0.22518      2.3653e+06          218.65          3.2376
v  total_pressure       4.8196e+05      6.4812e+05      5.9772e+05      5.7844e+05
v  Local Time Step            0.01        0.069599        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6069      2.5046e+06          544.13          71.098


 TIME FOR THE TIME STEP              588:        0.18243E+03

===============================================================


 INSTANT    0.589000000E+02   TIME STEP NUMBER             589
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet         v  Velocity[Z]             -12.581           8.626        -0.87764       -0.012342
v  ǁVelocityǁ             0.021032          16.286           5.181          6.1706
v  Pressure                 -18043      1.4812e+05           97723           78435
v  k                    2.9987e-07          4.1548        0.053097         0.07403
v  epsilon               0.0056927      7.7986e+05            1099          41.652
v  TurbVisc             5.6387e-13         0.41838       0.0024883        0.037579
v  CourantNb               0.15799       4.556e+05          325.48           67.86
v  FourierNb               0.22518      2.3653e+06          218.65          3.2376
v  total_pressure       4.8196e+05      6.4812e+05      5.9772e+05      5.7844e+05
v  Local Time Step            0.01        0.069599        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6069      2.5046e+06          544.13          71.098


 TIME FOR THE TIME STEP              588:        0.17743E+03

===============================================================


 INSTANT    0.589000000E+02   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         0.938261216E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969553E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13414E+02 0.46292E+01
   Friction velocity        uet   :  0.34309E-01 0.33867E+02
   Friction velocity        uk    :  0.33599E-01 0.33867E+02
   Dimensionless distance   yplus :  0.37044E-02 0.20248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11592
   Nb of faces within the viscous sub-layer     :      13006
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34581E+01     654   0.24209E+00   0.79737E+01 0.44303E+01 
c  Velocity[X]                                      0.21860E+01 
c  Velocity[Y]                                      0.37194E+01 
c  Velocity[Z]                                      0.20683E+01 
c  Pressure     0.11486E+00     977   0.11343E-01   0.31473E-01 0.60831E-01 
c  k            0.32023E+00     155   0.35958E-03   0.12953E-02 0.24569E+01 
c  epsilon      0.24175E+04      90   0.12061E-02   0.55576E+07 0.45204E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00055469                            65
a  epsilon                  -122.9                           157
a  Local Time Step      1.8335e-08                        281778


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.4953          12.094          1.3696          0.3248
v  Velocity[Y]             -9.7634          13.841          1.1253         0.77235
v  Velocity[Z]             -14.996          8.9696        -0.88214       -0.012449
v  ǁVelocityǁ             0.010229          17.154          5.1991          6.1715
v  Pressure                 -17964      1.4816e+05           97770           78479
v  k                    8.8743e-08          4.7298        0.052339        0.073951
v  epsilon              0.00015287      8.4991e+05          1041.2          41.554
v  TurbVisc             1.1175e-12         0.41838       0.0024686        0.037574
v  CourantNb                0.1536      5.4541e+05          321.97          67.933
v  FourierNb               0.22522      2.3653e+06          218.64          3.2358
v  total_pressure       4.8204e+05      6.4816e+05      5.9777e+05      5.7848e+05
v  Local Time Step            0.01        0.071063        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6007       2.671e+06          540.61          71.169


 TIME FOR THE TIME STEP              589:        0.20509E+03

===============================================================


 INSTANT    0.590000000E+02   TIME STEP NUMBER             590
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
-----------------------------------------------------------------------------
c  Velocity     0.34625E+01     597   0.24644E+00   0.91054E+01 0.47324E+01 
c  Velocity[X]                                      0.23927E+01 
c  Velocity[Y]                                      0.50619E+01 
c  Velocity[Z]                                      0.16508E+01 
c  Pressure     0.11246E+00     670   0.11242E-01   0.30813E-01 0.33970E-01 
c  k            0.32025E+00     146   0.27523E-03   0.12647E-02 0.24282E+01 
c  epsilon      0.25127E+04      89   0.16736E-02   0.46774E+07 0.43207E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0043857                            31
a  epsilon                 -51.268                            72
a  Local Time Step      1.5675e-08                        281779


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.7745          12.041          1.3617         0.32492
v  Velocity[Y]             -9.7222          14.684          1.1343         0.77254
v  Velocity[Z]             -14.351          10.227        -0.86734       -0.012762
v  ǁVelocityǁ             0.011552          16.971          5.2093          6.1743
v  Pressure                 ------------------------------------------------------------------------------
c  Velocity     0.34625E+01     597   0.24644E+00   0.91054E+01 0.47324E+01 
c  Velocity[X]                                      0.23927E+01 
c  Velocity[Y]                                      0.50619E+01 
c  Velocity[Z]                                      0.16508E+01 
c  Pressure     0.11246E+00     670   0.11242E-01   0.30813E-01 0.33970E-01 
c  k            0.32025E+00     146   0.27523E-03   0.12647E-02 0.24282E+01 
c  epsilon      0.25127E+04      89   0.16736E-02   0.46774E+07 0.43207E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0043857                            31
a  epsilon                 -51.268                            72
a  Local Time Step      1.5675e-08                        281779


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.7745          12.041          1.3617         0.32492
v  Velocity[Y]             -9.7222          14.684          1.1343         0.77254
v  Velocity[Z]             -14.351          10.227        -0.86734       -0.012762
v  ǁVelocityǁ             0.011552          16.971          5.2093          6.1743
v  Pressure                 -17948      1.4817e+05           97774           78482
v  k                    1.1329e-07          4.0612        0.053325        0.073845
v  epsilon              0.00014883      7.5475e+05          1115.1          41.569
v  TurbVisc             1.7808e-13         0.41838       0.0024728        0.037562
v  CourantNb               0.11768      6.3794e+05          325.98          67.976
v  FourierNb               0.22501      2.3653e+06          218.63          3.2342
v  total_pressure       4.8205e+05      6.4817e+05      5.9777e+05      5.7848e+05
v  Local Time Step            0.01         0.07817        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6044      2.7636e+06          544.61           71.21


 TIME FOR THE TIME STEP              590:        0.17032E+03

===============================================================


 INSTANT    0.591000000E+02   TIME STEP NUMBER             591
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
----------------------------------------------Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969567E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13336E+02 0.47062E+01
   Friction velocity        uet   :  0.17634E-01 0.51129E+02
   Friction velocity        uk    :  0.18373E-01 0.51129E+02
   Dimensionless distance   yplus :  0.31590E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11536
   Nb of faces within the viscous sub-layer     :      12970
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34610E+01     627   0.24838E+00   0.93825E+01 0.48073E+01 
c  Velocity[X]                                      0.26815E+01 
c  Velocity[Y]                                      0.50206E+01 
c  Velocity[Z]                                      0.16805E+01 
c  Pressure     0.11426E+00     905   0.11352E-01   0.31401E-01 0.39408E-01 
c  k            0.32030E+00     156   0.10617E-03   0.98982E-03 0.21479E+01 
c  epsilon      0.25872E+04      86   0.56134E-03   0.48646E+06 0.13818E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0015352                            17
a  epsilon                 -54.471                            31
a  Local Time Step       2.127e-08                        281777


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.7409          11.996           1.373          0.3239
v  Velocity[Y]             -9.7532          13.997          1.1109         0.77308
v  Velocity[Z]             -15.497          11.173        -0.87012       -0.013336
v  ǁVelocityǁ            0.0087712          17.547          5.1658          6.1709
v  Pressure                 -17990       1.482e+05           97761           78463
v  k                    3.0717e-07          4.2053        0.053153        0.073804
v  epsilon               0.0050221      7.9356e+05    Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969567E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13336E+02 0.47062E+01
   Friction velocity        uet   :  0.17634E-01 0.51129E+02
   Friction velocity        uk    :  0.18373E-01 0.51129E+02
   Dimensionless distance   yplus :  0.31590E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11536
   Nb of faces within the viscous sub-layer     :      12970
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34610E+01     627   0.24838E+00   0.93825E+01 0.48073E+01 
c  Velocity[X]                       Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969567E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13336E+02 0.47062E+01
   Friction velocity        uet   :  0.17634E-01 0.51129E+02
   Friction velocity        uk    :  0.18373E-01 0.51129E+02
   Dimensionless distance   yplus :  0.31590E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11536
   Nb of faces within the viscous sub-layer     :      12970
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34610E+01     627   0.24838E+00   0.93825E+01 0.48073E+01 
c  Velocity[X]                                      0.26815E+01 
c  Velocity[Y]                                      0.50206E+01 
c  Velocity[Z]                                      0.16805E+01 
c  Pressure     0.11426E+00     905   0.11352E-01   0.31401E-01 0.39408E-01 
c  k            0.32030E+00     156   0.10617E-03   0.98982E-03 0.21479E+01 
c  epsilon      0.25872E+04      86   0.56134E-03   0.48646E+06 0.13818E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0015352                            17
a  epsilon                 -54.471                            31
a  Local Time Step       2.127e-08                        281777


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.7409          11.996           1.373          0.3239
v  Velocity[Y]             -9.7532          13.997          1.1109         0.77308
v  Velocity[Z]             -15.497          11.173        -0.87012       -0.013336
v  ǁVelocityǁ            0.0087712     v  epsilon              8.7351e-05      7.6291e+05          1025.4          41.289
v  TurbVisc             1.4115e-12         0.41838       0.0024674        0.037539
v  CourantNb              0.015009       5.789e+05          320.82          67.901
v  FourierNb               0.22434      2.3653e+06          218.65          3.2351
v  total_pressure       4.8193e+05      6.4815e+05      5.9771e+05      5.7844e+05
v  Local Time Step            0.01         0.10404        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6628      2.7045e+06          539.47          71.136


 TIME FOR THE TIME STEP              593:        0.18881E+03

===============================================================


 INSTANT    0.594000000E+02   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         0.113326917E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969870E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13206E+02 0.46051E+01
   Friction velocity        uet   :  0.21252E-01 0.62330E+02
   Friction velocity        uk    :  0.21219E-01 0.62330E+02
   Dimensionless distance   yplus :  0.27635E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11545
   Nb of faces within the viscous sub-layer     :      13050
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34615E+01     613   0.23993E+00   0.10146E+02 0.49965E+01 
c  Velocity[X]                                      0.25881E+01 
c  Velocity[Y]                                      0.57781E+01 
c  Velocity[Z]                                      0.17802E+0v  epsilon              8.7351e-05      7.6291e+05          1025.4          41.289
v  TurbVisc             1.4115e-12         0.41838       0.0024674        0.037539
v  CourantNb              0.015009       5.789e+05          320.82          67.901
v  FourierNb               0.22434      2.3653e+06          218.65          3.2351
v  total_pressure       4.8193e+05      6.4815e+05      5.9771e+05      5.7844e+05
v  Local Time Step            0.01         0.10404        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6628      2.7045e+06          539.47          71.136


 TIME FOR THE TIME STEP              593:        0.18018E+03

===============================================================


 INSTANT    0.594000000E+02   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         0.113326917E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969870E+01
Free inlet               13 v  epsilon              8.7351e-05      7.6291e+05          1025.4          41.289
v  TurbVisc             1.4115e-12         0.41838       0.0024674        0.037539
v  CourantNb              0.015009       5.789e+05          320.82          67.901
v  FourierNb               0.22434      2.3653e+06          218.65          3.2351
v  total_pressure       4.8193e+05      6.4815e+05      5.9771e+05      5.7844e+05
v  Local Time Step            0.01         0.10404        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6628      2.7045e+06          539.47          71.136


 TIME FOR THE TIME STEP              593:        0.18520E+03

===============================================================


 INSTANT    0.594000000E+02   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         0.113326917E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969870E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13206E+02 0.46051E+01
   Friction velocity        uet   :  0.21252E-01 0.62330E+02
   Friction velocity        uk    :  0.21219E-01 0.62330E+02
   Dimensionless distance   yplus :  0.27635E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11545
   Nb of faces within the viscous sub-layer     :      13050
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34615E+01     613   0.23993E+00   0.10146E+02 0.49965E+01 
c  Velocity[X]                                      0.25881E+01 
c  Velocity[Y]                                      0.57781E+01 
c  Velocity[Z]                                      0.17802E+01 
c  Pressure     0.10709E+00     993   0.10890E-01   0.29466E-01 0.66112E-01 
c  k            0.32038E+00     141   0.10069E-03   0.91847E-03 0.20683E+01 
c  epsilon      0.24664E+04      87   0.49003E-03   0.34244E+06 0.12151E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00025113                            18
a  epsilon                 -62.618                            51
a  Local Time Step      1.5904e-08                        281780


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.8227          12.074          1.3579         0.32311
v  Velocity[Y]             -9.7383          14.657          1.1334         0.77207
v  Velocity[Z]             -14.623          8.8027        -0.86764       -0.013048
v  ǁVelocityǁ             0.020765          16.984             5.2          6.1737
v  Pressure                 -18135      1.4809e+05           97643           78394
v  k                    1.1297e-07          4.0543        0.052189        0.073966
v  epsilon              6.1311e-05      7.5318e+05          1046.1          41.364
v  TurbVisc             1.3719e-12         0.64915       0.0024562        0.037548
v  CourantNb              0.059858      6.2879e+05          322.57          67.956
v  FourierNb               0.22459      2.3653e+06          218.64          3.2351
v  total_pressure       4.8187e+05      6.4809e+05      5.9764e+05      5.7839e+05
v  Local Time Step            0.01         0.11445        0.010001        0.010009


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6984      2.7544e+06          541.21          71.191


 TIME FOR THE TIME STEP              594:        0.18192E+03

===============================================================


 INSTANT    0.595000000E+02   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         0.812512002E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3  c  Velocity[Z]                                      0.21145E+01 
c  Pressure     0.10967E+00     901   0.10746E-01   0.30164E-01 0.38661E-01 
c  k            0.32049E+00     142   0.10503E-03   0.97823E-03 0.21341E+01 
c  epsilon      0.25340E+04      88   0.79506E-03   0.71819E+06 0.17052E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0011147                            11
a  epsilon                  -36.93                            32
a  Local Time Step       2.511e-08                        281778


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.5415          12.179           1.352         0.32332
v  Velocity[Y]             -9.7055          14.174          1.1178         0.77165
v  Velocity[Z]             -14.329          11.254        -0.88412       -0.012807
v  ǁVelocityǁ            0.0096641          16.489          5.2224          6.1692
v  Pressure                 -18104      1.4815e+05           97678           78413
v  k                    1.4394e-07          4.2549        0.052552        0.074068
v  epsilon               0.0048303      8.1219e+05          1092.7          41.548
v  TurbVisc             3.0693e-13         0.41838       0.002459c  Velocity[Z]                                      0.21145E+01 
c  Pressure     0.10967E+00     901   0.10746E-01   0.30164E-01 0.38661E-01 
c  k            0.32049E+00     142   0.10503E-03   0.97823E-03 0.21341E+01 
c  epsilon      0.25340E+04      88   0.79506E-03   0.71819E+06 0.17052E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0011147                            11
a  epsilon                  -36.93                            32
a  Local Time Step       2.511e-08                        281778


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.5415          12.179           1.352         0.32332
v  Velocity[Y]             -9.7055          14.174          1.1178         0.77165
v  Velocity[Z]             -14.329          11.254        -0.88412       -0.012807
v  ǁVelocityǁ            0.0096641          16.489          5.2224          6.1692
v  Pressure                 -18104      1.4815e+05           97678           78413
v  k                    1.4394e-07          4.2549        0.052552        0.074068
v  epsilon               0.0048303      8.1219e+05          1092.7          41.548
v  TurbVisc             3.0693e-13         0.41838       0.0024596        0.037566
v  CourantNb               0.24654      3.9824e+05          323.04          67.964
v  FourierNb               0.22509      2.3653e+06          218.62           3.235
v  total_pressure        4.819e+05      6.4815e+05      5.9768e+05      5.7841e+05
v  Local Time Step            0.01         0.12527        0.010001        0.010009


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6585      2.5017e+06          541.65          71.199


 TIME FOR THE TIME STEP              595:        0.17588E+03

===============================================================


 INSTANT    0.596000000E+02   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        -0.856581083E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0       Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13209E+02 0.46894E+01
   Friction velocity        uet   :  0.38457E-01 0.39034E+02
   Friction velocity        uk    :  0.37376E-01 0.39034E+02
   Dimensionless distance   yplus :  0.35916E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11573
   Nb of faces within the viscous sub-layer     :      13029
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34607E+01     657   0.24615E+00   0.82037E+01 0.44948E+01 
c  Velocity[X]                                      0.23653E+01 
c  Velocity[Y]                                      0.36813E+01 
c  Velocity[Z]                                      0.21571E+01 
c  Pressure     0.10693E+00    1010   0.10356E-01   0.29357E-01 0.80612E-01 
c  k            0.32040E+00     155   0.10935E-03   0.12418E-02 0.24049E+01 
c  epsilon      0.25179E+04      97   0.85167E-03   0.90127E+06 0.19715E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.012743                           130
a  epsilon                 -1353.8                           250
a  Local Time Step      1.7478e-08                        281780


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -6.597          12.118          1.3871         0.32379
v  Velocity[Y]             -9.6001          13.992          1.1073         0.77247
v  Velocity[Z]             -14.904          9.9791        -0.85974       -0.012417
v  ǁVelocityǁ             0.013558          16.964          5.1812          6.1715
v  Pressure                 -17862       1.483e+05           97831           78560
v  k                    5.6154e-08          4.1504        0.052017        0.074131
v  epsilon              0.00087736      7.7969e+05            1035          41.517
v  TurbVisc             1.1016e-12         0.41838       0.0024867        0.037594
v  CourantNb              0.085787      5.7214e+05           321.6          67.898
v  FourierNb               0.22595      2.3653e+06          2Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13209E+02 0.46894E+01
   Friction velocity        uet   :  0.38457E-01 0.39034E+02
   Friction velocity        uk    :  0.37376E-01 0.39034E+02
   Dimensionless distance   yplus :  0.35916E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11573
   Nb of faces within the viscous sub-layer     :      13029
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34607E+01     657   0.24615E+00   0.82037E+01 0.44948E+01 
c  Velocity[X]                                      0.23653E+01 
c  Velocity[Y]                                      0.36813E+01 
c  Velocity[Z]                                      0.21571E+01 
c  Pressure     0.10693E+00    1010   0.10356E-01   0.29357E-01 0.80612E-01 
c  k            0.320Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13209E+02 0.46894E+01
   Friction velocity        uet   :  0.38457E-01 0.39034E+02
   Friction velocity        uk    :  0.37376E-01 0.39034E+02
   Dimensionless distance   yplus :  0.35916E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11573
   Nb of faces within the viscous sub-layer     :      13029
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34607E+01     657   0.24615E+00   0.82037E+01 0.44948E+01 
c  Velocity[X]                                      0.23653E+01 
c  Velocity[Y]                                      0.36813E+01 
c  Velocity[Z]                                      0.21571E+01 
c  Pressure     0.10693E+00    1010   0.10356E-01   0.29357E-01 0.80612E-01 
c  k            0.32040E+00     155   0.10935E-03   0.12418E-02 0.24049E+01 
c  epsilon      0.25179E+04      97   0.85167E-03   0.90127E+06 0.19715E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.012743                           130
a  epsilon                 -1353.8                           250
a  Local Time Step      1.7478e-08                        281780


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -6.597          12.118          1.3871         0.32379
v  Velocity[Y]             -9.6001          13.992          1.1073         0.77247
v  Velocity[Z]             -14.904          9.9791        -0.85974       -0.012417
v  ǁVelocityǁ             0.013558          16.964          5.1812          6.1715
v  Pressure                 -17862       1.483e+05           97831           78560
v  k                    5.6154e-08          4.1504        0.052017        0.074131
v  epsilon              0.00087736     v  FourierNb                0.2261      2.3653e+06          218.62           3.235
v  total_pressure       4.8219e+05      6.4833e+05      5.9784e+05      5.7856e+05
v  Local Time Step            0.01         0.11594        0.010001         0.01001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6418      2.6986e+06          540.75           71.22


 TIME FOR THE TIME STEP              598:        0.17393E+03

===============================================================


 INSTANT    0.599000000E+02   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         0.763412538E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969579E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13054E+02 0.46851E+01
   Friction velocity        uet   :  0.33603E-01 0.66567E+02
   Friction velocity        uk    :  0.34517E-01 0.66567E+02
   Dimensionless distance   yplus :  0.37573E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11602
   Nb of faces within the viscous sub-layer     :      13080
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34588E+01     592   0.24418E+00   0.82855E+01 0.45169E+01 
c  Velocity[X]                                      0.22593E+01 
c  Velocity[Y]                                      0.40883E+01 
c  Velocity[Z]                                      0.19378E+01 
c  Pressure     0.10793E+00     958   0.10718E-01   0.29570E-01 0.50856E-01 
c  k            0.32027E+00     150   0.11410E-03   0.10779E-02 0.22416E+01 
c  epsilon      0.25312E+04      87   0.68022E-03   0.64936E+06 0.16368E+02 
---------------v  FourierNb                0.2261      2.3653e+06          218.62           3.235
v  total_pressure       4.8219e+05      6.4833e+05      5.9784e+05      5.7856e+05
v  Local Time Step            0.01         0.11594        0.010001         0.01001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6418      2.6986e+06          540.75           71.22


 TIME FOR THE TIME STEP              598:        0.17015E+03

===============================================================


 INSTANT    0.599000000E+02   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         0.763412538E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969579E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------v  FourierNb                0.2261      2.3653e+06          218.62           3.235
v  total_pressure       4.8219e+05      6.4833e+05      5.9784e+05      5.7856e+05
v  Local Time Step            0.01         0.11594        0.010001         0.01001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6418      2.6986e+06          540.75           71.22


 TIME FOR THE TIME STEP              598:        0.17279E+03

===============================================================


 INSTANT    0.599000000E+02   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         0.763412538E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969579E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13054E+02 0.46851E+01
   Friction velocity        uet   :  0.33603E-01 0.66567E+02
   Friction velocity        uk    :  0.34517E-01 0.66567E+02
   Dimensionless distance   yplus :  0.37573E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11602
   Nb of faces within the viscous sub-layer     :      13080
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34588E+01     592   0.24418E+00   0.82855E+01 0.45169E+01 
c  Velocity[X]                                      0.22593E+01 
c  Velocity[Y]                                      0.40883E+01 
c  Velocity[Z]                                      0.19378E+01 
c  Pressure    Time for restart files:    0.14485E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34605E+01     611   0.24253E+00   0.91045E+01 0.47341E+01 
c  Velocity[X]                                      0.23782E+01 
c  Velocity[Y]                                      0.47951E+01 
c  Velocity[Z]                                      0.19312E+01 
c  Pressure     0.10436E+00     945   0.10019E-01   0.28610E-01 0.58253E-01 
c  k            0.32029E+00     143   0.14088E-03   0.11731E-02 0.23383E+01 
c  epsilon      0.26062E+04      93   0.13847E-02   0.14066E+07 0.23020E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00026689                             4
a  epsilon                 -60.186                            11
a  Local Time Step      2.0643e-08                        281781


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.7109          12.099          1.3743         0.32493
v  Velocity[Y]             -9.7261           13.98          1.1132         0.77317
v  Velocity[Z]              -15.24          8.6809        -0.86891       -0.013032
v  ǁVelocityǁ             0.011576          17.352          5.1643          6.1709
v  Pressure                 -17790      1.4847e+05           97938           78631
v  k                    1.9745e-07           4.301        0.053494        0.073883
v  epsilon               0.0050558       8.242e+05          1125.9          41.687
v  TurbVisc             4.7509e-13         0.41838       0.0024671        0.037564
v  CourantNb               0.22718      4.8442e+05          328.57          68.035
v  FourierNb               0.22537      2.3653e+06          218.63           3.234
v  total_pressure       4.8221e+05      6.4847e+05      5.9794e+05      5.7863e+05
v  Local Time Step            0.01        0.089388        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.614      2.5587e+06          547.21          71.269


 TIME FOR THE TIME STEP              600:        0.17941E+03

===============================================================


 INSTANT    0.601000000E+02   TIME STEP NUMBER             601
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
--------- Time for restart files:    0.14954E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34605E+01     611   0.24253E+00   0.91045E+01 0.47341E+01 
c  Velocity[X]                                      0.23782E+01 
c  Velocity[Y]                                      0.47951E+01 
c  Velocity[Z]                                      0.19312E+01 
c  Pressure     0.10436E+00     945   0.10019E-01   0.28610E-01 0.58253E-01 
c  k            0.32029E+00     143   0.14088E-03   0.11731E-02 0.23383E+01 
c  epsilon      0.26062E+04      93   0.13847E-02   0.14066E+07 0.23020E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00026689                             4
a  epsilon                 -60.186                            11
a  Local Time Step      2.0643e-08                        281781


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.7109          12.099          1.3743         0.32493
v  Velocity[Y]  Time for restart files:    0.12077E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34605E+01     611   0.24253E+00   0.91045E+01 0.47341E+01 
c  Velocity[X]                                      0.23782E+01 
c  Velocity[Y]                                      0.47951E+01 
c  Velocity[Z]                                      0.19312E+01 
c  Pressure     0.10436E+00     945   0.10019E-01   0.28610E-01 0.58253E-01 
c  k            0.32029E+00     143   0.14088E-03   0.11731E-02 0.23383E+01 
c  epsilon      0.26062E+04      93   0.13847E-02   0.14066E+07 0.23020E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00026689                             4
a  epsilon                 -60.186                            11
a  Local Time Step      2.0643e-08                        281781


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.7109          12.099          1.3743         0.32493
v  Velocity[Y]             -9.7261           13.98          1.1132         0.77317
v  Velocity[Z]              -15.24          8.6809        -0.86891       -0.013032
v  ǁVelocityǁ             0.011576          17.352          5.1643          6.1709
v  Pressure                 -17790      1.4847e+05           97938           78631
v  k                    1.9745e-07           4.301        0.053494        0.073883
v  epsilon               0.0050558       8.242e+05          1125.9          41.687
v  TurbVisc             4.7509e-13         0.41838       0.0024671        0.037564
v  CourantNb               0.22718      4.8442e+05          328.57          68.035
v  FourierNb               0.22537      2.3653e+06          218.63           3.234
v  total_pressure       4.8221e+05      6.4847e+05      5.9794e+05      5.7863e+05
v  Local Time Step            0.01        0.089388        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.614      2.5587e+06          547.21          71.269


 TIME FOR THE TIME STEP              600:        0.17449E+03

===============================================================


 INSTANT    0.601000000E+02   TIME STEP NUMBER             601
 ========================================================---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.802006094E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888703E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15125E+02 0.52564E+01
   Friction velocity        uet   :  0.32994E-01 0.47243E+02
   Friction velocity        uk    :  0.35717E-01 0.47243E+02
   Dimensionless distance   yplus :  0.56527E-02 0.23521E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12133
   Nb of faces within the viscous sub-layer     :      12756
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44119E+01     786   0.22299E+00   0.28136E+02 0.74363E+01 
c  Velocity[X]                                      0.59488E+01 
c  Velocity[Y]                                      0.91072E+01 
c  Velocity[Z]                                      0.13081E+02 
c  Pressure     0.25431E+00    1595   0.50225E-01   0.69243E-01 0.50634E+01 
c  k            0.51228E+00     313   0.51215E-03   0.36220E-01 0.91062E+01 
c  epsilon      0.29139E+04     200   0.20544E-02   0.42952E+07 0.36765E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012106                             8
a  epsilon                 -5.3693                            40
a  Local Time Step      2.0317e-08                        281775


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.4873          12.908          1.4628         0.38009
v  Velocity[Y]             -10.624          17.115          1.3096         0.89596
v  Velocity[Z]             -15.599          9.7059        -0.70419         0.11959
v  ǁVelocityǁ             0.026215          20.---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.802006094E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888703E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15125E+02 0.52564E+01
   Friction velocity        uet   :  0.32994E-01 0.47243E+02
   Friction velocity        uk    :  0.35717E-01 0.47243E+02
   Dimensionless distance   yplus :  0.56527E-02 0.23521E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12133
   Nb of faces within the viscous sub-layer     :      12756
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable   ---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.802006094E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888703E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15125E+02 0.52564E+01
   Friction velocity        uet   :  0.32994E-01 0.47243E+02
   Friction velocity        uk    :  0.35717E-01 0.47243E+02
   Dimensionless distance   yplus :  0.56527E-02 0.23521E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12133
   Nb of faces within the viscous sub-layer     :      12756
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44119E+01     786   0.22299E+00   0.28136E+02 0.74363E+01 
c  Velocity[X]                                      0.59488E+01 
c  Velocity[Y]                                      0.91072E+01 
c  Velocity[Z]                                      0.13081E+02 
c  Pressure     0.25431E+00    1595   0.50225E-01   0.69243E-01 0.50634E+01 
c  k            0.51228E+00     313   0.51215E-03   0.36220E-01 0.91062E+01 
c  epsilon      0.29139E+04     200   0.20544E-02   0.42952E+07 0.36765E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012106                             8
a  epsilon                 -5.3693                            40
a  Local Time Step      2.0317e-08                        281775


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.4873     v  ǁVelocityǁ            0.0073005          20.176          5.5154          6.9869
v  Pressure                -6384.6      1.7657e+05      1.2112e+05           97018
v  k                    1.8642e-07          4.0955        0.057056        0.099619
v  epsilon               0.0075298      7.6455e+05          1263.1          49.005
v  TurbVisc             6.2226e-13         0.49491       0.0029677        0.047043
v  CourantNb              0.082866      5.1455e+05          346.85          75.368
v  FourierNb               0.22511      2.3653e+06          218.67          3.3776
v  total_pressure       4.9362e+05      6.7657e+05      6.2112e+05      5.9702e+05
v  Local Time Step            0.01        0.022389            0.01        0.010001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2824      2.5539e+06          565.52          78.746


 TIME FOR THE TIME STEP              603:        0.23131E+03

===============================================================


 INSTANT    0.604000000E+02   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         0.588397042E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888731E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15553E+02 0.52689E+01
   Friction velocity        uet   :  0.39430E-01 0.55874E+02
   Friction velocity        uk    :  0.42261E-01 0.55874E+02
   Dimensionless distance   yplus :  0.71296E-02 0.23809E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12274
   Nb of faces within the viscous sub-layer     :      12321
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.v  ǁVelocityǁ            0.0073005          20.176          5.5154          6.9869
v  Pressure                -6384.6      1.7657e+05      1.2112e+05           97018
v  k                    1.8642e-07          4.0955        0.057056        0.099619
v  epsilon               0.0075298      7.6455e+05          1263.1          49.005
v  TurbVisc             6.2226e-13         0.49491       0.0029677        0.047043
v  CourantNb              0.082866      5.1455e+05          346.85          75.368
v  FourierNb               0.22511      2.3653e+06          218.67          3.3776
v  total_pressure       4.9362e+05      6.7657e+05      6.2112e+05      5.9702e+05
v  Local Time Step            0.01        0.022389            0.01        0.010001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2824      2.5539e+06          565.52          78.746


 TIME FOR THE TIME STEP              603:        0.23739E+03

===============================================================


 INSTANT    0.604000000E+02   TIME STEP NUMBER             604
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5      v  ǁVelocityǁ            0.0073005          20.176          5.5154          6.9869
v  Pressure                -6384.6      1.7657e+05      1.2112e+05           97018
v  k                    1.8642e-07          4.0955        0.057056        0.099619
v  epsilon               0.0075298      7.6455e+05          1263.1          49.005
v  TurbVisc             6.2226e-13         0.49491       0.0029677        0.047043
v  CourantNb              0.082866      5.1455e+05          346.85          75.368
v  FourierNb               0.22511      2.3653e+06          218.67          3.3776
v  total_pressure       4.9362e+05      6.7657e+05      6.2112e+05      5.9702e+05
v  Local Time Step            0.01        0.022389            0.01        0.010001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2824      2.5539e+06          565.52          78.746


 TIME FOR THE TIME STEP              603:        0.23023E+03

===============================================================


 INSTANT    0.604000000E+02   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         0.588397042E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888731E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15553E+02 0.52689E+01
   Friction velocity        uet   :  0.39430E-01 0.55874E+02
   Friction velocity        uk    :  0.42261E-01 0.55874E+02
   Dimensionless distance   yplus :  0.71296E-02 0.23809E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12274
   Nb of faces within the viscous sub-layer     :      12321
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
------------------------c  Velocity     0.44341E+01     742   0.23145E+00   0.12538E+02 0.48907E+01 
c  Velocity[X]                                      0.33458E+01 
c  Velocity[Y]                                      0.56503E+01 
c  Velocity[Z]                                      0.35414E+01 
c  Pressure     0.24413E+00    1496   0.41844E-01   0.64802E-01 0.25111E+01 
c  k            0.51069E+00     244   0.11222E-03   0.20077E-02 0.22090E+01 
c  epsilon      0.29419E+04     141   0.13539E-02   0.27271E+07 0.29922E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0072885                           210
a  epsilon                 -626.86                           365
a  Local Time Step       1.691e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.7739          12.343          1.5056          0.3687
v  Velocity[Y]             -9.9836          17.778          1.3851         0.88795
v  Velocity[Z]             -14.989          11.031        -0.94764       -0.024339
v  ǁVelocityǁ            0.0036819          20.432          5.5667          7.0295
v  Pressure                 -15691      1.7433e+05      1.1661e+05           92150
v  k                    1.8713e-07          4.2608        0.058929         0.10059
v  epsilon               0.0017092      8.0815e+05          1312.2          50.146
v  TurbVisc              6.434e-13         0.49488       0.0031127        0.047176
v  CourantNb              0.044192      5.9136e+05          353.76          75.788
v  FourierNb               0.22544      2.3653e+06           218.7          3.3943
v  total_pressure       4.8431e+05      6.7433e+05      6.1661e+05      5.9215e+05
v  Local Time Step            0.01        0.027091            0.01        0.010001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.1222      2.7169e+06          572.46          79.182


 TIME FOR THE TIME STEP              605:        0.22831E+03

===============================================================


 INSTANT    0.606000000E+02   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         0.123730155E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3     c  Velocity     0.44341E+01     742   0.23145E+00   0.12538E+02 0.48907E+01 
c  Velocity[X]                                      0.33458E+01 
c  Velocity[Y]                                      0.56503E+01 
c  Velocity[Z]                                      0.35414E+01 
c  Pressure     0.24413E+00    1496   0.41844E-01   0.64802E-01 0.25111E+01 
c  k            0.51069E+00     244   0.11222E-03   0.20077E-02 0.22090E+01 
c  epsilon      0.29419E+04     141   0.13539E-02   0.27271E+07 0.29922E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0072885                           210
a  epsilon                 -626.86                           365
a  Local Time Step       1.691e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.7739          12.343          1.5056          0.3687
v  Velocity[Y]             -9.9836          17.778          1.3851         0.88795
v  Velocity[Z]             -14.989          11.031        -0.94764       -0.024339
v  ǁVelocityǁ            0.0036819          20.432          5.5667          7.0295
v  Pressure                 -15691      1.7433e+05      1.1661e+05           92150
v  k                    c  Velocity     0.44341E+01     742   0.23145E+00   0.12538E+02 0.48907E+01 
c  Velocity[X]                                      0.33458E+01 
c  Velocity[Y]                                      0.56503E+01 
c  Velocity[Z]                                      0.35414E+01 
c  Pressure     0.24413E+00    1496   0.41844E-01   0.64802E-01 0.25111E+01 
c  k            0.51069E+00     244   0.11222E-03   0.20077E-02 0.22090E+01 
c  epsilon      0.29419E+04     141   0.13539E-02   0.27271E+07 0.29922E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0072885                           210
a  epsilon                 -626.86                           365
a  Local Time Step       1.691e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.7739          12.343          1.5056          0.3687
v  Velocity[Y]             -9.9836          17.778          1.3851         0.88795
v  Velocity[Z]             -14.989          11.031        -0.94764       -0.024339
v  ǁVelocityǁ            0.0036819          20.432          5.5667          7.0295
v  Pressure                 -15691      1.7433e+05      1.1661e+05           92150
v  k                    1.8713e-07          4.2608        0.058929         0.10059
v  epsilon               0.0017092      8.0815e+05          1312.2          50.146
v  TurbVisc              6.434e-13         0.49488       0.0031127        0.047176
v  CourantNb              0.044192      5.9136e+05          353.76          75.788
v  FourierNb               0.22544      2.3653e+06           218.7          3.3943
v  total_pressure       4.8431e+05      6.7433e+05      6.1661e+05      5.9215e+05
v  Local Time Step            0.01        0.027091            0.01        0.010001


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.1222      2.7169e+06          572.46          79.182


 TIME FOR THE TIME STEP              605:        0.22521E+03

===============================================================


 INSTANT    0.606000000E+02   TIME STEP NUMBER             606
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46       Free outlet               3          46         0.312889079E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15418E+02 0.52687E+01
   Friction velocity        uet   :  0.24651E-01 0.63286E+02
   Friction velocity        uk    :  0.24371E-01 0.63286E+02
   Dimensionless distance   yplus :  0.77588E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12520
   Nb of faces within the viscous sub-layer     :      12087
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44128E+01     705   0.23072E+00   0.86599E+01 0.40681E+01 
c  Velocity[X]                                      0.22754E+01 
c  Velocity[Y]                                      0.42428E+01 
c  Velocity[Z]                                      0.21417E+01 
c  Pressure     0.21063E+00    1342   0.34459E-01   0.55030E-01 0.81237E+00 
c  k            0.51073E+00     213   0.94246E-04   0.12095E-02 0.17150E+01 
c  epsilon      0.30129E+04     110   0.71633E-03   0.11873E+07 0.19387E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0005135                            42
a  epsilon                 -126.09                            54
a  Local Time Step      2.0372e-08                        281775


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.9232          12.282          1.5172         0.36639
v  Velocity[Y]             -10.288          17.209          1.3935          0.8805
v  Velocity[Z]             -14.918          11.174         -1.0185       -0.027449
v  ǁVelocityǁ             0.013896          19.821          5.6519          7.0205
v  Pressure                 -21724      1.7211e+05      1.1313e+05           89577
v  k                    8.0065e-08          4.1925        0.060192         0.10062
v  epsilon               0.0026949      7.8742e+05          1345.9          50.698
v  TurbVisc             8.1211e-14 Free outlet               3          46         0.312889079E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15418E+02 0.52687E+01
   Friction velocity        uet   :  0.24651E-01 0.63286E+02
   Friction velocity        uk    :  0.24371E-01 0.63286E+02
   Dimensionless distance   yplus :  0.77588E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12520
   Nb of faces within the viscous sub-layer     :      12087
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44128E+01     705   0.23072E+00   0.86599E+01 0.40681E+01 
c  Velocity[X]                                      0.22754E+01 
c  Velocity[Y]                      Free outlet               3          46         0.312889079E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15418E+02 0.52687E+01
   Friction velocity        uet   :  0.24651E-01 0.63286E+02
   Friction velocity        uk    :  0.24371E-01 0.63286E+02
   Dimensionless distance   yplus :  0.77588E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12520
   Nb of faces within the viscous sub-layer     :      12087
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44128E+01     705   0.23072E+00   0.86599E+01 0.40681E+01 
c  Velocity[X]                                      0.22754E+01 
c  Velocity[Y]                                      0.42428E+01 
c  Velocity[Z]                                      0.21417E+01 
c  Pressure     0.21063E+00    1342   0.34459E-01   0.55030E-01 0.81237E+00 
c  k            0.51073E+00     213   0.94246E-04   0.12095E-02 0.17150E+01 
c  epsilon      0.30129E+04     110   0.71633E-03   0.11873E+07 0.19387E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0005135                            42
a  epsilon                 -126.09                            54
a  Local Time Step      2.0372e-08                        281775


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.9232          12.282          1.5172         0.36639
v  Velocity[Y]             -10.288          17.209          1.3935          0.8805
v  Velocity[Z]             -14.918          11.174         -1.0185       -0.027449
v  ǁVelocityǁ             0.013896          19.821          5.6519          7.0205
v  Pressure                 -21724     v  TurbVisc             2.7692e-13         0.49487        0.003206        0.047299
v  CourantNb             0.0047169      4.8473e+05          356.25          76.273
v  FourierNb               0.22583      2.3653e+06          218.76          3.4031
v  total_pressure       4.7732e+05      6.7263e+05       6.131e+05      5.8989e+05
v  Local Time Step            0.01        0.036058            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.90348      2.4837e+06          575.02          79.676


 TIME FOR THE TIME STEP              608:        0.18886E+03

===============================================================


 INSTANT    0.609000000E+02   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         0.680158262E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888754E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15307E+02 0.52684E+01
   Friction velocity        uet   :  0.31809E-01 0.33241E+02
   Friction velocity        uk    :  0.34991E-01 0.33241E+02
   Dimensionless distance   yplus :  0.24398E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12520
   Nb of faces within the viscous sub-layer     :      12018
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44082E+01     688   0.22820E+00   0.80047E+01 0.39148E+01 
c  Velocity[X]                                      0.20352E+01 
c  Velocity[Y]                                      0.40724E+01 
c  Velocity[Z]                                      0.18971E+01 
c  Pressure     0.19228E+00    1321   0.30080E-01   0.49508E-01 0.86466E+00 
c  v  TurbVisc             2.7692e-13         0.49487        0.003206        0.047299
v  CourantNb             0.0047169      4.8473e+05          356.25          76.273
v  FourierNb               0.22583      2.3653e+06          218.76          3.4031
v  total_pressure       4.7732e+05      6.7263e+05       6.131e+05      5.8989e+05
v  Local Time Step            0.01        0.036058            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.90348      2.4837e+06          575.02          79.676


 TIME FOR THE TIME STEP              608:        0.19582E+03

===============================================================


 INSTANT    0.609000000E+02   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         0.680158262E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888754E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0        v  TurbVisc             2.7692e-13         0.49487        0.003206        0.047299
v  CourantNb             0.0047169      4.8473e+05          356.25          76.273
v  FourierNb               0.22583      2.3653e+06          218.76          3.4031
v  total_pressure       4.7732e+05      6.7263e+05       6.131e+05      5.8989e+05
v  Local Time Step            0.01        0.036058            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.90348      2.4837e+06          575.02          79.676


 TIME FOR THE TIME STEP              608:        0.18820E+03

===============================================================


 INSTANT    0.609000000E+02   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         0.680158262E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888754E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15307E+02 0.52684E+01
   Friction velocity        uet   :  0.31809E-01 0.33241E+02
   Friction velocity        uk    :  0.34991E-01 0.33241E+02
   Dimensionless distance   yplus :  0.24398E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12520
   Nb of faces within the viscous sub-layer     :      12018
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44082E+01     688   0.22820E+00   0.80047E+01 0.39148E+01 
c  Velocity[X]                                      0.20352E+01 
c  Velocity[Y]                                      0.40724E+01 
c  Velocity[Z]                                      0.18971E+01 
c  Pressure     0.19228E+00    1321   0.30080E-01   0.49508E-01 0.86466E+00 
c  k            0.51072E+00     189   0.65481E-04   0.93816E-03 0.15102E+01 
c  epsilon      0.29730E+04     100   0.41359E-03   0.59816E+06 0.14059E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0037363                            23
a  epsilon                 -289.57                            79
a  Local Time Step      2.2414e-08                        281768


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.9271          12.375          1.5323           0.369
v  Velocity[Y]             -10.002          16.739          1.2957          0.8844
v  Velocity[Z]             -14.878          9.8433         -0.9578        -0.01278
v  ǁVelocityǁ             0.014641          19.186          5.6455          7.0106
v  Pressure                 -22810      1.7381e+05      1.1379e+05           90789
v  k                    2.9497e-07            4.19        0.060039         0.10072
v  epsilon              0.00080075      7.8697e+05            1300            50.7
v  TurbVisc             1.1052e-12         0.49487       0.0032131         0.04731
v  CourantNb              0.028817      4.4616e+05          355.46          76.315
v  FourierNb               0.22585      2.3653e+06          218.79          3.4019
v  total_pressure       4.7719e+05      6.7381e+05      6.1379e+05      5.9079e+05
v  Local Time Step            0.01        0.039664            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2995      2.5717e+06          574.25          79.717


 TIME FOR THE TIME STEP              609:        0.21303E+03

===============================================================


 INSTANT    0.610000000E+02   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        -0.150660337E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888700E+01
Free inlet               13   c  Pressure     0.18882E+00    1370   0.28359E-01   0.48262E-01 0.11110E+01 
c  k            0.51072E+00     161   0.64001E-04   0.95574E-03 0.15240E+01 
c  epsilon      0.29460E+04      99   0.47298E-03   0.56900E+06 0.13698E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.004906                            30
a  epsilon                 -110.58                            73
a  Local Time Step      2.4833e-08                        281780


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.9312          12.355          1.5256         0.37071
v  Velocity[Y]             -10.199          16.678          1.2948         0.88583
v  Velocity[Z]             -14.665          12.245        -0.94863      -0.0083519
v  ǁVelocityǁ             0.015071          19.253          5.6495          7.0104
v  Pressure                 -22440      1.7538e+05      1.1492e+05           92001
v  k                     7.288e-08           4.117        0.060128         0.10077
v  epsilon              0.00076632      7.6758e+05          1302.8          50.765
v  TurbVisc             1.3098e-12         0.49487       0.0032202        0.047319
v  CourantNb               0.27539      4.0269ec  Pressure     0.18882E+00    1370   0.28359E-01   0.48262E-01 0.11110E+01 
c  k            0.51072E+00     161   0.64001E-04   0.95574E-03 0.15240E+01 
c  epsilon      0.29460E+04      99   0.47298E-03   0.56900E+06 0.13698E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.004906                            30
a  epsilon                 -110.58                            73
a  Local Time Step      2.4833e-08                        281780


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.9312          12.355          1.5256         0.37071
v  Velocity[Y]             -10.199          16.678          1.2948         0.88583
v  Velocity[Z]             -14.665          12.245        -0.94863      -0.0083519
v  ǁVelocityǁ             0.015071          19.253          5.6495          7.0104
v  Pressure                 -22440      1.7538e+05      1.1492e+05           92001
v  k                     7.288e-08           4.117        0.060128         0.10077
v  epsilon              0.00076632      7.6758e+05          1302.8          50.765
v  TurbVisc             1.3098e-12         0.49487       0.0032202        0.047319
v  CourantNb               0.27539      4.0269e+05          353.05          76.328
v  FourierNb               0.22589      2.3653e+06          218.79          3.4036
v  total_pressure       4.7756e+05      6.7538e+05      6.1492e+05        5.92e+05
v  Local Time Step            0.01        0.040175            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4279      2.4875e+06          571.84          79.732


 TIME FOR THE TIME STEP              610:        0.20969E+03

===============================================================


 INSTANT    0.611000000E+02   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        -0.424674212E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46       Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15769E+02 0.52680E+01
   Friction velocity        uet   :  0.35614E-01 0.50010E+02
   Friction velocity        uk    :  0.41035E-01 0.50010E+02
   Dimensionless distance   yplus :  0.63814E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12543
   Nb of faces within the viscous sub-layer     :      12179
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44284E+01     605   0.23227E+00   0.66766E+01 0.35673E+01 
c  Velocity[X]                                      0.20925E+01 
c  Velocity[Y]                                      0.28089E+01 
c  Velocity[Z]                                      0.17752E+01 
c  Pressure     0.18091E+00    1340   0.25154E-01   0.45444E-01 0.84878E+00 
c  k            0.51073E+00     174   0.53666E-04   0.91310E-03 0.14895E+01 
c  epsilon      0.28812E+04      94   0.40030E-03   0.74108E+06 0.15884E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0021882                            28
a  epsilon                  -13.52                            51
a  Local Time Step       2.105e-08                        281781


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0544           12.75          1.5686         0.37059
v  Velocity[Y]             -10.039          16.638          1.2774         0.88917
v  Velocity[Z]             -14.466           10.45        -0.90515      -0.0080478
v  ǁVelocityǁ              0.01823          19.147          5.6516           7.022
v  Pressure                 -21599      1.7817e+05      1.1705e+05           94058
v  k                    4.2307e-07          4.1297        0.059431         0.10095
v  epsilon              0.00068196      7.7195e+05          1262.8          50.699
v  TurbVisc             9.3457e-13         0.49487         0.00322         0.04734
v  CourantNb              0.069791      4.7505e+05          352.03          76.412
v  FourierNb                0.2264      2.3653e+06          218.78          3.4031
v  total_pressure        4.784e+05      6.Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15769E+02 0.52680E+01
   Friction velocity        uet   :  0.35614E-01 0.50010E+02
   Friction velocity        uk    :  0.41035E-01 0.50010E+02
   Dimensionless distance   yplus :  0.63814E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12543
   Nb of faces within the viscous sub-layer     :      12179
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44284E+01     605   0.23227E+00   0.66766E+01 0.35673E+01 
c  Velocity[X]                                      0.20925E+01 
c  Velocity[Y]                                      0.28089E+01 
c  Velocity[Z]                                      0.17752E+01 
c  Pressure     0.18091E+00    1340   0.25154E-01   0.45444E-01 0.84878E+00 
c  k            0.51073E+00     174   0.53666E-04   0.91310E-03 0.14895E+01 
c  epsilUndefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15769E+02 0.52680E+01
   Friction velocity        uet   :  0.35614E-01 0.50010E+02
   Friction velocity        uk    :  0.41035E-01 0.50010E+02
   Dimensionless distance   yplus :  0.63814E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12543
   Nb of faces within the viscous sub-layer     :      12179
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44284E+01     605   0.23227E+00   0.66766E+01 0.35673E+01 
c  Velocity[X]                                      0.20925E+01 
c  Velocity[Y]                                      0.28089E+01 
c  Velocity[Z]                                      0.17752E+01 
c  Pressure     0.18091E+00    1340   0.25154E-01   0.45444E-01 0.84878E+00 
c  k            0.51073E+00     174   0.53666E-04   0.91310E-03 0.14895E+01 
c  epsilon      0.28812E+04      94   0.40030E-03   0.74108E+06 0.15884E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0021882                            28
a  epsilon                  -13.52                            51
a  Local Time Step       2.105e-08                        281781


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0544           12.75          1.5686         0.37059
v  Velocity[Y]             -10.039          16.638          1.2774         0.88917
v  Velocity[Z]             -14.466           10.45        -0.90515      -0.0080478
v  ǁVelocityǁ              0.01823          19.147          5.6516           7.022
v  Pressure                 -21599      1.7817e+05      1.1705e+05           94058
v  k                    4.2307e-07          4.1297        0.059431         0.10095
v  epsilon              0.00068196      7.7195e+05          1262.8          50.699
v  TurbVisc             9.3457e-13     v  total_pressure       4.7865e+05      6.7928e+05      6.1792e+05      5.9481e+05
v  Local Time Step            0.01        0.026177            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6734      2.5672e+06          570.43          79.915


 TIME FOR THE TIME STEP              613:        0.20267E+03

===============================================================


 INSTANT    0.614000000E+02   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         0.128554046E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888731E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15929E+02 0.52678E+01
   Friction velocity        uet   :  0.35340E-01 0.45487E+02
   Friction velocity        uk    :  0.46758E-01 0.45487E+02
   Dimensionless distance   yplus :  0.58042E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12567
   Nb of faces within the viscous sub-layer     :      12269
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44382E+01     616   0.23169E+00   0.68070E+01 0.35949E+01 
c  Velocity[X]                                      0.22384E+01 
c  Velocity[Y]                                      0.29049E+01 
c  Velocity[Z]                                      0.16637E+01 
c  Pressure     0.16938E+00    1317   0.21925E-01   0.41857E-01 0.63982E+00 
c  k            0.51078E+00     156   0.67043E-04   0.10199E-02 0.15735E+01 
c  epsilon      0.29208E+04     101   0.61455E-03   0.49574E+06 0.12768E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippingv  total_pressure       4.7865e+05      6.7928e+05      6.1792e+05      5.9481e+05
v  Local Time Step            0.01        0.026177            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6734      2.5672e+06          570.43          79.915


 TIME FOR THE TIME STEP              613:        0.19535E+03

===============================================================


 INSTANT    0.614000000E+02   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         0.128554046E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888731E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH Wv  total_pressure       4.7865e+05      6.7928e+05      6.1792e+05      5.9481e+05
v  Local Time Step            0.01        0.026177            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6734      2.5672e+06          570.43          79.915


 TIME FOR THE TIME STEP              613:        0.19942E+03

===============================================================


 INSTANT    0.614000000E+02   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         0.128554046E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888731E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15929E+02 0.52678E+01
   Friction velocity        uet   :  0.35340E-01 0.45487E+02
   Friction velocity        uk    :  0.46758E-01 0.45487E+02
   Dimensionless distance   yplus :  0.58042E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12567
   Nb of faces within the viscous sub-layer     :      12269
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44382E+01     616   0.23169E+00   0.68070E+01 0.35949E+01 
c  Velocity[X]                                      0.22384E+01 
c  Velocity[Y]                                      0.29049E+01 
c  Velocity[Z]                                      0.16637E+01 
c  Pressure     0.16938E+00    1317   0.21925E-01   0.41857E-01 0.63982E+00 
c  k            0.51078E+00     156   0.67043E-04   0.10199E-02 0.15735E+01 
c  epsilon      0.29208E+04     101   0.61455E-03   0.49574E+06 0.12768E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0041211                            49
a  epsilon                 -104.17                           130
a  Local Time Step      2.3645e-08                        281786


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0008          13.086          1.5356         0.37198
v  Velocity[Y]             -10.258          16.863          1.2876         0.89043
v  Velocity[Z]             -14.026          9.7919        -0.94008       -0.011763
v  ǁVelocityǁ             0.017437          19.383          5.6922          7.0336
v  Pressure                 -21205      1.8028e+05      1.1872e+05           95440
v  k                    1.0384e-07          4.2059        0.059683         0.10115
v  epsilon              1.2726e-05      7.9935e+05          1286.1          51.032
v  TurbVisc             9.5258e-13         0.49487       0.0032203        0.047365
v  CourantNb                0.1659      4.2292e+05             352          76.618
v  FourierNb               0.22657      2.3653e+06          218.76          3.4042
v  total_pressure       4.7879e+05      6.8028e+05      6.1872e+05      5.9544e+05
v  Local Time Step            0.01        0.028794            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6604      2.4931e+06          570.76          80.022


 TIME FOR THE TIME STEP              614:        0.19147E+03

===============================================================


 INSTANT    0.615000000E+02   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         0.142470733E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888712E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIO
  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.9455e-06                             1
a  epsilon                 -21.954                             9
a  Local Time Step      2.0974e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.9161          13.205          1.5701         0.37202
v  Velocity[Y]             -10.285           16.56            1.28         0.89193
v  Velocity[Z]             -14.145           11.58         -0.9348       -0.013948
v  ǁVelocityǁ             0.005123          19.027          5.6807          7.0387
v  Pressure                 -21254      1.8093e+05      1.1921e+05           95796
v  k                    3.5781e-07          5.9552         0.05976         0.10126
v  epsilon               0.0050109      1.7398e+06            1313          51.183
v  TurbVisc             9.0463e-13         0.49487       0.0032249        0.047375
v  CourantNb               0.27441      4.7678e+05          354.98          76.688
v  FourierNb               0.22654      2.3653e+06          218.76          3.4037
v  total_pressure       4.7875e+05      6.8093e+05      6.1921e+05       5.958e+05
v  Local Time Step            0.01        0.031674            0.01        0.010003


  ** Computed values on cell
  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.9455e-06                             1
a  epsilon                 -21.954                             9
a  Local Time Step      2.0974e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.9161          13.205          1.5701         0.37202
v  Velocity[Y]             -10.285           16.56            1.28         0.89193
v  Velocity[Z]             -14.145           11.58         -0.9348       -0.013948
v  ǁVelocityǁ             0.005123          19.027          5.6807          7.0387
v  Pressure                 -21254      1.8093e+05      1.1921e+05           95796
v  k                    3.5781e-07          5.9552         0.05976         0.10126
v  epsilon               0.0050109      1.7398e+06            1313          51.183
v  TurbVisc             9.0463e-13         0.49487       0.0032249        0.047375
v  CourantNb               0.27441      4.7678e+05          354.98          76.688
v  FourierNb               0.22654      2.3653e+06          218.76          3.4037
v  total_pressure       4.7875e+05      6.8093e+05      6.1921e+05       5.958e+05
v  Local Time Step            0.01        0.031674            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6541      2.6024e+06          573.74          80.091


 TIME FOR THE TIME STEP              615:        0.19207E+03

===============================================================


 INSTANT    0.616000000E+02   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        -0.134400306E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888693E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15977E+02 0.52675E+01
   Friction velocity        uet   :  0.37622E-01 0.42091E+02
   Friction velocity        uk    :  0.46440E-01 0.42091E+02
   Dimensionless distance   yplus :  0.15127E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12604
   Nb of faces within the viscous sub-layer     :      12217
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44456E+01     628   0.23027E+00   0.96056E+01 0.42601E+01 
c  Velocity[X]                                      0.22591E+01 
c  Velocity[Y]                                      0.54380E+01 
c  Velocity[Z]                                      0.19085E+01 
c  Pressure     0.15779E+00    1195   0.19698E-01   0.38166E-01 0.32962E+00 
c  k            0.51086E+00     171   0.83764E-04   0.13084E-02 0.17809E+01 
c  epsilon      0.29861E+04     101   0.49423E-03   0.58818E+06 0.13815E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00055225                             5
a  epsilon                 -9.2958                            21
a  Local Time Step      2.0051e-08                        281786


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.9499          13.316          1.5453         0.37299
v  Velocity[Y]             -10.458          16.477          1.2657         0.89239
v  Velocity[Z]             -14.133          10.043         -0.9517        -0.01582
v  ǁVelocityǁ             0.021393           18.89          5.7234          7.0518
v  Pressure                 -21684      1.8182e+05       1.198e+05           96167
v  k                    3.4806e-07          4.2647        0.060174          0.1014
v  epsilon              0.00082035      1.0118e+06          1288.3          51.536
v  TurbVisc              1.083e-12         0.49487       0.0032304        0.047393
v  CourantNb              0.041997      4.9873e+05          355.18          76.922
v  FourierNb               0.22625      2.3653e+06          218.76          3.4049
v  total_pressure       4.7832e+05      6.8182e+05       6.198e+05      5.9617e+05
v  Local Time Step            0.01        0.038325            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  ------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15977E+02 0.52675E+01
   Friction velocity        uet   :  0.37622E-01 0.42091E+02
   Friction velocity        uk    :  0.46440E-01 0.42091E+02
   Dimensionless distance   yplus :  0.15127E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12604
   Nb of faces within the viscous sub-layer     :      12217
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44456E+01     628   0.23027E+00   0.96056E+01 0.42601E+01 
c  Velocity[X]                                      0.22591E+01 
c  Velocity[Y]                                      0.54380E+01 
c  Velocity[Z]                                      0.19085E+01 
c  Pressure     0.15779E+00    1195   0.19698E-01   0.38166E-01 0.32962E+00 
c  k            0.51086E+00     171   0.83764E-04   0.13084E-02 0.17809E+01 
c  epsilon      0.29861E+04     101   0.49423E-03   0.58818E+06 0.13815E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15977E+02 0.52675E+01
   Friction velocity        uet   :  0.37622E-01 0.42091E+02
   Friction velocity        uk    :  0.46440E-01 0.42091E+02
   Dimensionless distance   yplus :  0.15127E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12604
   Nb of faces within the viscous sub-layer     :      12217
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44456E+01     628   0.23027E+00   0.96056E+01 0.42601E+01 
c  Velocity[X]                                      0.22591E+01 
c  Velocity[Y]                                      0.54380E+01 
c  Velocity[Z]                                      0.19085E+01 
c  Pressure     0.15779E+00    1195   0.19698E-01   0.38166E-01 0.32962E+00 
c  k            0.51086E+00     171   0.83764E-04   0.13084E-02 0.17809E+01 
c  epsilon      0.29861E+04     101   0.49423E-03   0.58818E+06 0.13815E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00055225                             5
a  epsilon                 -9.2958                            21
a  Local Time Step      2.0051e-08                        281786


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.9499          13.316          1.5453         0.37299
v  Velocity[Y]             -10.458          16.477          1.2657         0.89239
v  Velocity[Z]             -14.133          10.043         -0.9517        -0.01582
v  ǁVelocityǁ             0.021393           18.89          5.7234          7.0518
v  Pressure                 -21684      1.8182e+05       1.198e+05           96167
v  k                    3.4806e-07          4.2647        0.060174          0.1014
v  epsilon              0.00082035      1.0118e+06          1288.3          51.536
v  TurbVisc              1.083e-12         0.49487       0.0032304        0.047393
v  CourantNb              0.041997      4.9873e+05          355.18          76.922
v  FourierNb               0.22625      2.3653e+06          218.76          3.4049
v  total_pressure       4.7832e+05      6.8182e+05       6.198e+05      5.9617e+05
v  Local Time Step    ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.662      2.5705e+06          574.39          80.424


 TIME FOR THE TIME STEP              618:        0.19375E+03

===============================================================


 INSTANT    0.619000000E+02   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         0.258200559E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888722E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16132E+02 0.52675E+01
   Friction velocity        uet   :  0.38418E-01 0.39330E+02
   Friction velocity        uk    :  0.43609E-01 0.39330E+02
   Dimensionless distance   yplus :  0.46655E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12586
   Nb of faces within the viscous sub-layer     :      12181
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44586E+01     634   0.23451E+00   0.98080E+01 0.43015E+01 
c  Velocity[X]                                      0.24297E+01 
c  Velocity[Y]                                      0.55004E+01 
c  Velocity[Z]                                      0.18779E+01 
c  Pressure     0.14910E+00    1042   0.18105E-01   0.35643E-01 0.20942E+00 
c  k            0.51090E+00     164   0.60884E-04   0.10691E-02 0.16096E+01 
c  epsilon      0.30672E+04      95   0.69705E-03   0.59250E+06 0.13484E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00018589                            11
a  epsilon                 -10.   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.662      2.5705e+06          574.39          80.424


 TIME FOR THE TIME STEP              618:        0.19201E+03

===============================================================


 INSTANT    0.619000000E+02   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         0.258200559E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888722E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16132E+02 0.52675E+01
   Friction velocity   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.662      2.5705e+06          574.39          80.424


 TIME FOR THE TIME STEP              618:        0.19240E+03

===============================================================


 INSTANT    0.619000000E+02   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         0.258200559E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888722E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16132E+02 0.52675E+01
   Friction velocity        uet   :  0.38418E-01 0.39330E+02
   Friction velocity        uk    :  0.43609E-01 0.39330E+02
   Dimensionless distance   yplus :  0.46655E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12586
   Nb of faces within the viscous sub-layer     :      12181
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44586E+01     634   0.23451E+00   0.98080E+01 0.43015E+01 
c  Velocity[X]                                      0.24297E+01 
c  Velocity[Y]                                      0.55004E+01 
c  Velocity[Z]                                      0.18779E+01 
c  Pressure     0.14910E+00    1042   0.18105E-01   0.35643E-01 0.20942E+00 
c  k            0.51090E+00     164   0.60884E-04   0.10691E-02 0.16096E+01 
c  epsilon      0.30672E+04      95   0.69705E-03   0.59250E+06 0.13484E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field     a  epsilon                 -104.22                            37
a  Local Time Step      1.5468e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.8597           13.24          1.5741         0.37148
v  Velocity[Y]             -10.623          15.862           1.219         0.89041
v  Velocity[Z]             -13.589          10.629        -0.93418       -0.016239
v  ǁVelocityǁ            0.0053399          18.326          5.7625           7.062
v  Pressure                 -22255      1.8286e+05      1.2041e+05           96475
v  k                    6.6628e-08          4.3607        0.060208         0.10134
v  epsilon              0.00062962      1.0502e+06          1298.1          51.518
v  TurbVisc             1.0787e-12         0.49487       0.0032389        0.047378
v  CourantNb              0.030605       6.465e+05          354.29          76.993
v  FourierNb               0.22566      2.3653e+06          218.79          3.4067
v  total_pressure       4.7774e+05      6.8286e+05      6.2041e+05      5.9648e+05
v  Local Time Step            0.01        0.041474            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5812      2.7721e+06          573.09            80.4


 TIME FOR THE TIME STEP              620:        0.18114E+03

===============================================================


 INSTANT    0.621000000E+02   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        -0.592483427E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888681E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15932E+02 0.52672E+01
   Friction velocity        uet   :  0.26931E-01 0.38929E+02
   Friction velocity        uk    :  0.38918E-01 0.38929E+02
   Dimensionless distance   yplus :  0.16627E-02 0.23856E+02
   ------------a  epsilon                 -104.22                            37
a  Local Time Step      1.5468e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.8597           13.24          1.5741         0.37148
v  Velocity[Y]             -10.623          15.862           1.219         0.89041
v  Velocity[Z]             -13.589          10.629        -0.93418       -0.016239
v  ǁVelocityǁ            0.0053399          18.326          5.7625           7.062
v  Pressure                 -22255      1.8286e+05      1.2041e+05           96475
v  k                    6.6628e-08          4.3607        0.060208         0.10134
v  epsilon              0.00062962      1.0502e+06          1298.1          51.518
v  TurbVisc             1.0787e-12         0.49487       0.0032389        0.047378
v  CourantNb              0.030605       6.465e+05          354.29          76.993
v  FourierNb               0.22566      2.3653e+06          218.79          3.4067
v  total_pressure       4.7774e+05      6.8286e+05      6.2041e+05      5.9648e+05
v  Local Time Step            0.01        0.041474            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5812      2.7721e+06          573.09            80.4


 TIME FOR Ta  epsilon                 -104.22                            37
a  Local Time Step      1.5468e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.8597           13.24          1.5741         0.37148
v  Velocity[Y]             -10.623          15.862           1.219         0.89041
v  Velocity[Z]             -13.589          10.629        -0.93418       -0.016239
v  ǁVelocityǁ            0.0053399          18.326          5.7625           7.062
v  Pressure                 -22255      1.8286e+05      1.2041e+05           96475
v  k                    6.6628e-08          4.3607        0.060208         0.10134
v  epsilon              0.00062962      1.0502e+06          1298.1          51.518
v  TurbVisc             1.0787e-12         0.49487       0.0032389        0.047378
v  CourantNb              0.030605       6.465e+05          354.29          76.993
v  FourierNb               0.22566      2.3653e+06          218.79          3.4067
v  total_pressure       4.7774e+05      6.8286e+05      6.2041e+05      5.9648e+05
v  Local Time Step            0.01        0.041474            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5812      2.7721e+06          573.09            80.4


 TIME FOR THE TIME STEP              620:        0.18457E+03

===============================================================


 INSTANT    0.621000000E+02   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        -0.592483427E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888681E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn    ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12716
   Nb of faces within the viscous sub-layer     :      12096
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44624E+01     601   0.23447E+00   0.89856E+01 0.41148E+01 
c  Velocity[X]                                      0.23669E+01 
c  Velocity[Y]                                      0.43767E+01 
c  Velocity[Z]                                      0.22420E+01 
c  Pressure     0.14732E+00    1157   0.16847E-01   0.34793E-01 0.24794E+00 
c  k            0.51093E+00     174   0.86976E-04   0.14765E-02 0.18921E+01 
c  epsilon      0.31076E+04      96   0.78519E-03   0.10519E+07 0.17656E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0058142                            62
a  epsilon                 -80.713                           204
a  Local Time Step      2.0606e-08                        281787


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.8594          13.392          1.5437         0.36974
v  Velocity[Y]              -10.64          15.332          1.2755         0.88704
v  Velocity[Z]             -14.215          9.8144        -0.95228         -0.0165
v  ǁVelocityǁ              0.01459          17.772          5.7694          7.0604
v  Pressure                 -22419      1.8364e+05      1.2094e+05           96778
v  k                    4.3127e-07          4.5126        0.061549         0.10134
v  epsilon               0.0004576      1.0747e+06          1367.7          52.017
v  TurbVisc             1.0982e-12         0.49487       0.0032342        0.047367
v  CourantNb               0.20547      4.8529e+05          359.99          77.271
v  FourierNb               0.22552      2.3653e+06          218.82          3.4065
v  total_pressure       4.7758e+05      6.8364e+05      6.2094e+05      5.9678e+05
v  Local Time Step            0.01        0.050184            0.01        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6101      2.6109e+06          578.81          80.677


 TIME FOR THE TIME STEP              622:        0.17932E+03

===============================================================


 INSTANT    0.623000000E+02   TIME STEP NUMBER             623
 =============   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12716
   Nb of faces within the viscous sub-layer     :      12096
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44624E+01     601   0.23447E+00   0.89856E+01 0.41148E+01 
c  Velocity[X]                                      0.23669E+01 
c  Velocity[Y]                                      0.43767E+01 
c  Velocity[Z]                                      0.22420E+01 
c  Pressure     0.14732E+00    1157   0.16847E-01   0.34793E-01 0.24794E+00 
c  k            0.51093E+00     174   0.86976E-04   0.14765E-02 0.18921E+01 
c  epsilon      0.31076E+04      96   0.78519E-03   0.10519E+07 0.17656E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0058142                            62
a  epsilon                 -80.713                           204
a  Local Time Step      2.0606e-08                        281787


  ** Computed fields on cells
     ------------------------

     ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12716
   Nb of faces within the viscous sub-layer     :      12096
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44624E+01     601   0.23447E+00   0.89856E+01 0.41148E+01 
c  Velocity[X]                                      0.23669E+01 
c  Velocity[Y]                                      0.43767E+01 
c  Velocity[Z]                                      0.22420E+01 
c  Pressure     0.14732E+00    1157   0.16847E-01   0.34793E-01 0.24794E+00 
c  k            0.51093E+00     174   0.86976E-04   0.14765E-02 0.18921E+01 
c  epsilon      0.31076E+04      96   0.78519E-03   0.10519E+07 0.17656E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0058142                            62
a  epsilon                 -80.713                           204
a  Local Time Step      2.0606e-08                        281787


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.8594          13.392          1.5437         0.36974
v  Velocity[Y]              -10.64          15.332          1.2755         0.88704
v  Velocity[Z]             -14.215          9.8144        -0.95228         -0.0165
v  ǁVelocityǁ              0.01459          17.772          5.7694          7.0604
v  Pressure                 -22419      1.8364e+05      1.2094e+05           96778
v  k                    4.3127e-07          4.5126        0.061549         0.10134
v  epsilon               0.0004576      1.0747e+06          1367.7          52.017
v  TurbVisc             1.0982e-12         0.49487       0.0032342        0.047367
v  CourantNb               0.20547      4.8529e+05          359.99          77.271
v  FourierNb               0.22552      2.3653e+06          218.82          3.4065
v  total_pressure       4.7758e+05      6.8364e+05      6.2094e+05      5.9678e+05
v  Local Time Step            0.01        0.050184            0.01        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6101      2.6109e+06          578.81 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.180460883E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888713E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15756E+02 0.52672E+01
   Friction velocity        uet   :  0.36133E-01 0.53556E+02
   Friction velocity        uk    :  0.35709E-01 0.53556E+02
   Dimensionless distance   yplus :  0.22560E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12699
   Nb of faces within the viscous sub-layer     :      12138
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44613E+01     608   0.23567E+00   0.91674E+01 0.41530E+01 
c  Velocity[X]                                      0.25881E+01 
c  Velocity[Y]                                      0.41976E+01 
c  Velocity[Z]                                      0.23817E+01 
c  Pressure     0.14410E+00    1106   0.16326E-01   0.33846E-01 0.18665E+00 
c  k            0.51091E+00     159   0.73095E-04   0.13437E-02 0.18049E+01 
c  epsilon      0.30821E+04     110   0.43303E-03   0.52484E+06 0.12622E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0010008                             5
a  epsilon                  -3.093                            23
a  Local Time Step      1.4252e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.8 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.180460883E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888713E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15756E+02 0.52672E+01
   Friction velocity        uet   :  0.36133E-01 0.53556E+02
   Friction velocity        uk    :  0.35709E-01 0.53556E+02
   Dimensionless distance   yplus :  0.22560E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12699
   Nb of faces within the viscous sub-layer     :      12138
   Total number  ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.180460883E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888713E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15756E+02 0.52672E+01
   Friction velocity        uet   :  0.36133E-01 0.53556E+02
   Friction velocity        uk    :  0.35709E-01 0.53556E+02
   Dimensionless distance   yplus :  0.22560E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12699
   Nb of faces within the viscous sub-layer     :      12138
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44613E+01     608   0.23567E+00   0.91674E+01 0.41530E+01 
c  Velocity[X]                                      0.25881E+01 
c  Velocity[Y]                                      0.41976E+01 
c  Velocity[Z]                                      0.23817E+01 
c  Pressure     0.14410E+00    1106   0.16326E-01   0.33846E-01 0.18665E+00 
c  k            0.51091E+00     159   0.73095E-04   0.13437E-02 0.18049E+01 
c  epsilon      0.30821E+04     110   0.43303E-03   0.52484E+06 0.12622E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0010008                             5
a  epsilon                  -3.093                            23
a  Local Time Step      1.4252e-08                        281784


  ** Computed fiev  Velocity[X]             -6.8606          13.366          1.5354         0.37035
v  Velocity[Y]             -10.627          15.401          1.3004         0.88565
v  Velocity[Z]              -16.92           9.522        -0.97508       -0.014904
v  ǁVelocityǁ             0.013536          19.363          5.8316          7.0732
v  Pressure                 -22556      1.8444e+05      1.2151e+05           97168
v  k                    4.1954e-07          4.6136         0.06187         0.10137
v  epsilon               0.0052186      1.0159e+06          1373.5           52.15
v  TurbVisc             9.1567e-13         0.49487        0.003228        0.047358
v  CourantNb               0.13839      5.2997e+05          360.11          77.383
v  FourierNb               0.22554      2.3653e+06          218.82          3.4053
v  total_pressure       4.7744e+05      6.8444e+05      6.2151e+05      5.9717e+05
v  Local Time Step            0.01        0.066795            0.01        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5754      2.6555e+06          578.93          80.788


 TIME FOR THE TIME STEP              625:        0.19059E+03

===============================================================


 INSTANT    0.626000000E+02   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         0.791512170E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888699E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15549E+02 0.52671E+01
   Friction velocity        uet   :  0.10756E-01 0.35239E+02
   Friction velocity        uk    :  0.40255E-01 0.35239E+02
   Dimensionless distance   yplus :  0.35547E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12758
   Nb of faces within the viscous sub-layer     :      12018
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---v  Velocity[X]             -6.8606          13.366          1.5354         0.37035
v  Velocity[Y]             -10.627          15.401          1.3004         0.88565
v  Velocity[Z]              -16.92           9.522        -0.97508       -0.014904
v  ǁVelocityǁ             0.013536          19.363          5.8316          7.0732
v  Pressure                 -22556      1.8444e+05      1.2151e+05           97168
v  k                    4.1954e-07          4.6136         0.06187         0.10137
v  epsilon               0.0052186      1.0159e+06          1373.5           52.15
v  TurbVisc             9.1567e-13         0.49487        0.003228        0.047358
v  CourantNb               0.13839      5.2997e+05          360.11          77.383
v  FourierNb               0.22554      2.3653e+06          218.82          3.4053
v  total_pressure       4.7744e+05      6.8444e+05      6.2151e+05      5.9717e+05
v  Local Time Step            0.01        0.066795            0.01        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5754      2.6555e+06          578.93          80.788


 TIME FOR THE TIME STEP              625:        0.18529E+03

===============================================================


 INSTANT    0.626000000E+02   TIME STEP NUMBER             626
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

------------------------------------v  Velocity[X]             -6.8606          13.366          1.5354         0.37035
v  Velocity[Y]             -10.627          15.401          1.3004         0.88565
v  Velocity[Z]              -16.92           9.522        -0.97508       -0.014904
v  ǁVelocityǁ             0.013536          19.363          5.8316          7.0732
v  Pressure                 -22556      1.8444e+05      1.2151e+05           97168
v  k                    4.1954e-07          4.6136         0.06187         0.10137
v  epsilon               0.0052186      1.0159e+06          1373.5           52.15
v  TurbVisc             9.1567e-13         0.49487        0.003228        0.047358
v  CourantNb               0.13839      5.2997e+05          360.11          77.383
v  FourierNb               0.22554      2.3653e+06          218.82          3.4053
v  total_pressure       4.7744e+05      6.8444e+05      6.2151e+05      5.9717e+05
v  Local Time Step            0.01        0.066795            0.01        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5754      2.6555e+06          578.93          80.788


 TIME FOR THE TIME STEP              625:        0.18901E+03

===============================================================


 INSTANT    0.626000000E+02   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         0.791512170E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888699E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15549E+02 0.52671E+01
   Friction velocity        uet   :  0.10756E-01 0.35239E+02
   Friction velocity        uk    :  0.40255E-01 0.35239E+02
   Dimensionless distance   yplus :  0.35547E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12758
   Nb of       --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44682E+01     610   0.23695E+00   0.10507E+02 0.44402E+01 
c  Velocity[X]                                      0.31059E+01 
c  Velocity[Y]                                      0.57286E+01 
c  Velocity[Z]                                      0.16728E+01 
c  Pressure     0.13126E+00    1125   0.13544E-01   0.30476E-01 0.21192E+00 
c  k            0.51111E+00     164   0.82275E-04   0.10970E-02 0.16300E+01 
c  epsilon      0.32212E+04      97   0.59777E-03   0.68861E+06 0.13820E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0022085                            22
a  epsilon                 -23.978                            49
a  Local Time Step      1.3623e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -6.986           13.52           1.566         0.37289
v  Velocity[Y]             -10.633          14.884          1.2518         0.88898
v  Velocity[Z]             -15.755          11.652         -0.9594       -0.015321
v  ǁVelocityǁ             0.016942          18.276           5.788          7.0766
v  Pressure                 -22571      1.8517e+05      1.2206e+05           97646
v  k                    2.3931e-07          5.1054        0.062343          0.1015
v  epsilon               0.0010697      1.0912e+06          1418.4          52.366
v  TurbVisc             1.0827e-12         0.49487       0.0032406         0.04737
v  CourantNb               0.17633      7.3407e+05          366.42          77.438
v  FourierNb               0.22552      2.3653e+06          218.87          3.4043
v  total_pressure       4.7743e+05      6.8517e+05      6.2206e+05      5.9765e+05
v  Local Time Step            0.01        0.062367        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6288      2.8597e+06          585.28          80.843


 TIME FOR THE TIME STEP              627:        0.18407E+03

===============================================================


 INSTANT    0.628000000E+02   TIME STEP NUMBER             628
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44682E+01     610   0.23695E+00   0.10507E+02 0.44402E+01 
c  Velocity[X]                                      0.31059E+01 
c  Velocity[Y]                                      0.57286E+01 
c  Velocity[Z]                                      0.16728E+01 
c  Pressure     0.13126E+00    1125   0.13544E-01   0.30476E-01 0.21192E+00 
c  k            0.51111E+00     164   0.82275E-04   0.10970E-02 0.16300E+01 
c  epsilon      0.32212E+04      97   0.59777E-03   0.68861E+06 0.13820E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0022085                            22
a  epsilon                 -23.978                            49
a  Local Time Step      1.3623e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -6.986           13.52           1.566         0.37289
v  Velocity[Y]             -10.633          14.884          1.2518         0.88898
v  Veloc      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44682E+01     610   0.23695E+00   0.10507E+02 0.44402E+01 
c  Velocity[X]                                      0.31059E+01 
c  Velocity[Y]                                      0.57286E+01 
c  Velocity[Z]                                      0.16728E+01 
c  Pressure     0.13126E+00    1125   0.13544E-01   0.30476E-01 0.21192E+00 
c  k            0.51111E+00     164   0.82275E-04   0.10970E-02 0.16300E+01 
c  epsilon      0.32212E+04      97   0.59777E-03   0.68861E+06 0.13820E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0022085                            22
a  epsilon                 -23.978                            49
a  Local Time Step      1.3623e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -6.986           13.52           1.566         0.37289
v  Velocity[Y]             -10.633          14.884          1.2518         0.88898
v  Velocity[Z]             -15.755          11.652         -0.9594       -0.015321
v  ǁVelocityǁ             0.016942          18.276           5.788          7.0766
v  Pressure                 -22571      1.8517e+05      1.2206e+05           97646
v  k                    2.3931e-07          5.1054        0.062343          0.1015
v  epsilon               0.0010697      1.0912e+06          1418.4          52.366
v  TurbVisc             1.0827e-12         0.49487       0.0032406         0.04737
v  CourantNb               0.17633      7.3407e+05          366.42          77.438
v  FourierNb               0.22552      2.3653e+06          218.87          3.4043
v  total_pressure       4.7743e+05      6.8517e+05      6.2206e+05      5.9765e+05
v  Local Time Step            0.01        0.062367        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6288      2.8597e+06          585.28          80.843


 TIME FOR THE TIME STEP              627:        0.18375E+03

===============================================================


 INSTANT    0.628000000E+02   TIME STEP NUMBER             628
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ----------Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.986721346E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888713E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15479E+02 0.52670E+01
   Friction velocity        uet   :  0.37290E-01 0.31544E+02
   Friction velocity        uk    :  0.39624E-01 0.31544E+02
   Dimensionless distance   yplus :  0.20265E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12804
   Nb of faces within the viscous sub-layer     :      11934
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44643E+01     613   0.24212E+00   0.11016E+02 0.45421E+01 
c  Velocity[X]                                      0.27822E+01 
c  Velocity[Y]                                      0.64369E+01 
c  Velocity[Z]                                      0.17966E+01 
c  Pressure     0.12498E+00    1125   0.12652E-01   0.28820E-01 0.20495E+00 
c  k            0.51121E+00     159   0.85048E-04   0.16771E-02 0.20146E+01 
c  epsilon      0.31667E+04     106   0.56500E-03   0.72229E+06 0.14293E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00073211                             5
a  epsilon                 -11.639                             5
a  Local Time Step      1.8349e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.8664          13.471          1.5469         0.37445
v  Velocity[Y]             -10.773          15.073          1.3108         0.89027
v  Velocity[Z]             -15.524          10.631         -0.9964       -0.013734
v  ǁVelocityǁ            0.0038484          17.989          5.8758          7.0837
v  Pressure                 Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.986721346E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888713E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15479E+02 0.52670E+01
   Friction velocity        uet   :  0.37290E-01 0.31544E+02
   Friction velocity        uk    :  0.39624E-01 0.31544E+02
   Dimensionless distance   yplus :  0.20265E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12804
   Nb of faces within the viscous sub-layer     :      11934
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.986721346E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888713E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15479E+02 0.52670E+01
   Friction velocity        uet   :  0.37290E-01 0.31544E+02
   Friction velocity        uk    :  0.39624E-01 0.31544E+02
   Dimensionless distance   yplus :  0.20265E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12804
   Nb of faces within the viscous sub-layer     :      11934
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44643E+01     613   0.24212E+00   0.11016E+02 0.45421E+01 
c  Velocity[X]                                      0.27822E+01 
c  Velocity[Y]                                      0.64369E+01 
c  Velocity[Z]                                      0.17966E+01 
c  Pressure     0.12498E+00    1125   0.12652E-01   0.28820E-01 0.20495E+00 
c  k            0.51121E+00     159   0.85048E-04   0.16771E-02 0.20146E+01 
c  epsilon      0.31667E+04     106   0.56500E-03   0.72229E+06 0.14293E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00073211                             5
a  epsilon                 -11.639                             5
a  Local Time Step      1.8349e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.8664          13.471          1.5469         0.37445
v  Velocity[Y]             -10.773       v  Pressure                 -22540      1.8622e+05      1.2287e+05           98408
v  k                    4.9277e-08          4.8237        0.063683          0.1017
v  epsilon               0.0012874      1.0879e+06            1458           52.97
v  TurbVisc             1.2591e-12         0.49487         0.00324        0.047383
v  CourantNb              0.014577      6.8134e+05           369.3           77.64
v  FourierNb               0.22546      2.3653e+06           218.9          3.4047
v  total_pressure       4.7746e+05      6.8622e+05      6.2287e+05      5.9841e+05
v  Local Time Step            0.01        0.075821        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6469      2.8069e+06           588.2          81.044


 TIME FOR THE TIME STEP              630:        0.19948E+03

===============================================================


 INSTANT    0.631000000E+02   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         0.225834547E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888721E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15535E+02 0.52820E+01
   Friction velocity        uet   :  0.36510E-01 0.43598E+02
   Friction velocity        uk    :  0.47287E-01 0.43598E+02
   Dimensionless distance   yplus :  0.41429E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12804
   Nb of faces within the viscous sub-layer     :      11969
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44719E+01     627   0.23409E+00   0.11483E+02 0.46373E+01 
c  Velocity[X]            v  Pressure                 -22540      1.8622e+05      1.2287e+05           98408
v  k                    4.9277e-08          4.8237        0.063683          0.1017
v  epsilon               0.0012874      1.0879e+06            1458           52.97
v  TurbVisc             1.2591e-12         0.49487         0.00324        0.047383
v  CourantNb              0.014577      6.8134e+05           369.3           77.64
v  FourierNb               0.22546      2.3653e+06           218.9          3.4047
v  total_pressure       4.7746e+05      6.8622e+05      6.2287e+05      5.9841e+05
v  Local Time Step            0.01        0.075821        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6469      2.8069e+06           588.2          81.044


 TIME FOR THE TIME STEP              630:        0.19030E+03

===============================================================


 INSTANT    0.631000000E+02   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         0.225834547E-16
Rough wall                6           0         0.0000v  Pressure                 -22540      1.8622e+05      1.2287e+05           98408
v  k                    4.9277e-08          4.8237        0.063683          0.1017
v  epsilon               0.0012874      1.0879e+06            1458           52.97
v  TurbVisc             1.2591e-12         0.49487         0.00324        0.047383
v  CourantNb              0.014577      6.8134e+05           369.3           77.64
v  FourierNb               0.22546      2.3653e+06           218.9          3.4047
v  total_pressure       4.7746e+05      6.8622e+05      6.2287e+05      5.9841e+05
v  Local Time Step            0.01        0.075821        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6469      2.8069e+06           588.2          81.044


 TIME FOR THE TIME STEP              630:        0.19095E+03

===============================================================


 INSTANT    0.631000000E+02   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         0.225834547E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888721E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15535E+02 0.52820E+01
   Friction velocity        uet   :  0.36510E-01 0.43598E+02
   Friction velocity        uk    :  0.47287E-01 0.43598E+02
   Dimensionless distance   yplus :  0.41429E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12804
   Nb of faces within the viscous sub-layer     :      11969
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44719E+01     627   0.23409E+00   0.11483E+02 0.46373E+01 
c  Velocity[X]                                      0.31566E+01 
c  Velocity[Y]                                      0.63220E+01 
c  Velocity[Z]                                      0.20041E+01 
c  Pressure     0.13606E+00    1149   0.13003E-01   0.31180E-01 0.19462E+00 
c  k            0.51112E+00     156   0.86126E-04   0.18556E-02 0.21198E+01 
c  epsilon      0.32598E+04      93   0.12095E-02   0.17088E+07 0.21239E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0040696                            11
a  epsilon                 -149.11                            19
a  Local Time Step      1.5014e-08                        281781


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.9995          13.555          1.5539         0.37571
v  Velocity[Y]              -10.66           15.38          1.2694          0.8933
v  Velocity[Z]             -16.673          9.6052        -0.97346       -0.014555
v  ǁVelocityǁ             0.012748          19.109          5.8343          7.0835
v  Pressure                 -22531      1.8653e+05      1.2311e+05           98634
v  k                    9.8911e-08          5.0131        0.063232         0.10165
v  epsilon              0.00014244      1.1116e+06          1467.5          52.757
v  TurbVisc             8.9472e-13         0.49487       0.0032449        0.047391
v  CourantNb               0.26634      6.6604e+05          369.19          77.617
v  FourierNb               0.22554      2.3653e+06          218.89           3.405
v  total_pressure       4.7747e+05      6.8653e+05      6.2311e+05      5.9863e+05
v  Local Time Step            0.01        0.083403        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6247      2.7916e+06          588.08          81.022


 TIME FOR THE TIME STEP              631:        0.18966E+03

===============================================================


 INSTANT    0.632000000E+02   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         0.157883388E-16
Rough wall                6c  Velocity[X]                                      0.25702E+01 
c  Velocity[Y]                                      0.35068E+01 
c  Velocity[Z]                                      0.23605E+01 
c  Pressure     0.13573E+00    1117   0.12984E-01   0.31004E-01 0.17087E+00 
c  k            0.51102E+00     170   0.79058E-04   0.14204E-02 0.18550E+01 
c  epsilon      0.31918E+04     109   0.10123E-02   0.15410E+07 0.20800E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.010313                            18
a  epsilon                 -277.22                            33
a  Local Time Step       1.812e-08                        281786


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.8698          13.491          1.5516          0.3762
v  Velocity[Y]             -10.688          15.055          1.2784         0.89442
v  Velocity[Z]             -17.829          9.8155        -0.99142       -0.013349
v  ǁVelocityǁ            0.0081331          20.218          5.8718          7.0855
v  Pressure                 -22556       1.868e+05      1.2332e+05           98832
v  k                     2.265e-07           4.809        0.063219         0.10159
v  epsilon        c  Velocity[X]                                      0.25702E+01 
c  Velocity[Y]                                      0.35068E+01 
c  Velocity[Z]                                      0.23605E+01 
c  Pressure     0.13573E+00    1117   0.12984E-01   0.31004E-01 0.17087E+00 
c  k            0.51102E+00     170   0.79058E-04   0.14204E-02 0.18550E+01 
c  epsilon      0.31918E+04     109   0.10123E-02   0.15410E+07 0.20800E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.010313                            18
a  epsilon                 -277.22                            33
a  Local Time Step       1.812e-08                        281786


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.8698          13.491          1.5516          0.3762
v  Velocity[Y]             -10.688          15.055          1.2784         0.89442
v  Velocity[Z]             -17.829          9.8155        -0.99142       -0.013349
v  ǁVelocityǁ            0.0081331          20.218          5.8718          7.0855
v  Pressure                 -22556       1.868e+05      1.2332e+05           98832
v  k                     2.265e-07           4.809        0.063219         0.10159
v  epsilon               0.0018255      1.0894e+06          1424.2          52.797
v  TurbVisc             8.3855e-13         0.49487       0.0032474        0.047386
v  CourantNb              0.080637      5.5188e+05          364.54          77.568
v  FourierNb               0.22545      2.3653e+06          218.89          3.4055
v  total_pressure       4.7744e+05       6.868e+05      6.2332e+05      5.9883e+05
v  Local Time Step            0.01        0.089819        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5957      2.6774e+06          583.42          80.974


 TIME FOR THE TIME STEP              632:        0.19585E+03

===============================================================


 INSTANT    0.633000000E+02   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       Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15790E+02 0.52670E+01
   Friction velocity        uet   :  0.39293E-01 0.54195E+02
   Friction velocity        uk    :  0.43693E-01 0.54195E+02
   Dimensionless distance   yplus :  0.34690E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12845
   Nb of faces within the viscous sub-layer     :      11860
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44733E+01     634   0.23629E+00   0.99929E+01 0.43215E+01 
c  Velocity[X]                                      0.28438E+01 
c  Velocity[Y]                                      0.48053E+01 
c  Velocity[Z]                                      0.23439E+01 
c  Pressure     0.13659E+00    1114   0.13283E-01   0.30980E-01 0.15124E+00 
c  k            0.51100E+00     163   0.69407E-04   0.80368E-03 0.13954E+01 
c  epsilon      0.32207E+04     101   0.89218E-03   0.85737E+06 0.15201E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00068546                            17
a  epsilon                  -20.47                            25
a  Local Time Step       1.352e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1673          13.679          1.5491         0.37627
v  Velocity[Y]             -10.666          15.362          1.3214         0.89528
v  Velocity[Z]             -18.455          10.028        -0.97929       -0.015349
v  ǁVelocityǁ             0.016857           20.78          5.9164          7.0916
v  Pressure                 -22812      1.8733e+05      1.2372e+05           99184
v  k                    3.5518e-07          4.8776        0.064345          0.1015
v  epsilon               0.0058414       1.099e+06            1483          52.952
v  TurbVisc             4.8757e-13         0.49487        0.003245        0.047368
v  CourantNb    Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15790E+02 0.52670E+01
   Friction velocity        uet   :  0.39293E-01 0.54195E+02
   Friction velocity        uk    :  0.43693E-01 0.54195E+02
   Dimensionless distance   yplus :  0.34690E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12845
   Nb of faces within the viscous sub-layer     :      11860
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44733E+01     634   0.23629E+00   0.99929E+01 0.43215E+01 
c  Velocity[X]                                      0.28438E+01 
c  Velocity[Y]                                      0.48053E+01 
c  Velocity[Z]                     Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15790E+02 0.52670E+01
   Friction velocity        uet   :  0.39293E-01 0.54195E+02
   Friction velocity        uk    :  0.43693E-01 0.54195E+02
   Dimensionless distance   yplus :  0.34690E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12845
   Nb of faces within the viscous sub-layer     :      11860
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44733E+01     634   0.23629E+00   0.99929E+01 0.43215E+01 
c  Velocity[X]                                      0.28438E+01 
c  Velocity[Y]                                      0.48053E+01 
c  Velocity[Z]                                      0.23439E+01 
c  Pressure     0.13659E+00    1114   0.13283E-01   0.30980E-01 0.15124E+00 
c  k            0.51100E+00     163   0.69407E-04   0.80368E-03 0.13954E+01 
c  epsilon      0.32207E+04     101   0.89218E-03   0.85737E+06 0.15201E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00068546                            17
a  epsilon                  -20.47                            25
a  Local Time Step       1.352e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1673          13.679          1.5491         0.37627
v  Velocity[Y]             -10.666          15.362          1.3214         0.89528
v  Velocity[Z]             -18.455          10.028        -0.97929       -0.015349
v  ǁVelocityǁ             0.016857           20.78          5.9164          7.0916
v  Pressure                 -22812      1.8733e+05      1.2372e+05           99184
v  k                    3.5518e-07     v  CourantNb              0.049881      6.1825e+05          373.23          77.782
v  FourierNb               0.22503      2.3653e+06          218.91          3.4045
v  total_pressure       4.7695e+05      6.8742e+05      6.2379e+05      5.9924e+05
v  Local Time Step            0.01         0.10578        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5939      2.7438e+06          592.14          81.187


 TIME FOR THE TIME STEP              635:        0.17422E+03

===============================================================


 INSTANT    0.636000000E+02   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         0.323864418E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888701E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15859E+02 0.52826E+01
   Friction velocity        uet   :  0.32881E-01 0.21824E+02
   Friction velocity        uk    :  0.32848E-01 0.21824E+02
   Dimensionless distance   yplus :  0.27848E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12868
   Nb of faces within the viscous sub-layer     :      11869
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44742E+01     610   0.23608E+00   0.85564E+01 0.39974E+01 
c  Velocity[X]                                      0.25728E+01 
c  Velocity[Y]                                      0.39652E+01 
c  Velocity[Z]                                      0.20184E+01 
c  Pressure     0.13047E+00     901   0.12529E-01   0.29439E-01 0.58971E-01 
c  k            0.51095E+00     179   0.62957E-04   0.92451E-03 0.14967E+01 
c  epsilov  CourantNb              0.049881      6.1825e+05          373.23          77.782
v  FourierNb               0.22503      2.3653e+06          218.91          3.4045
v  total_pressure       4.7695e+05      6.8742e+05      6.2379e+05      5.9924e+05
v  Local Time Step            0.01         0.10578        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5939      2.7438e+06          592.14          81.187


 TIME FOR THE TIME STEP              635:        0.18477E+03

===============================================================


 INSTANT    0.636000000E+02   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         0.323864418E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888701E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Unv  CourantNb              0.049881      6.1825e+05          373.23          77.782
v  FourierNb               0.22503      2.3653e+06          218.91          3.4045
v  total_pressure       4.7695e+05      6.8742e+05      6.2379e+05      5.9924e+05
v  Local Time Step            0.01         0.10578        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5939      2.7438e+06          592.14          81.187


 TIME FOR THE TIME STEP              635:        0.18538E+03

===============================================================


 INSTANT    0.636000000E+02   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         0.323864418E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888701E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15859E+02 0.52826E+01
   Friction velocity        uet   :  0.32881E-01 0.21824E+02
   Friction velocity        uk    :  0.32848E-01 0.21824E+02
   Dimensionless distance   yplus :  0.27848E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12868
   Nb of faces within the viscous sub-layer     :      11869
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44742E+01     610   0.23608E+00   0.85564E+01 0.39974E+01 
c  Velocity[X]                                      0.25728E+01 
c  Velocity[Y]                                      0.39652E+01 
c  Velocity[Z]                                      0.20184E+01 
c  Pressure     0.13047E+00     901   0.12529E-01   0.29439E-01 0.58971E-01 
c  k            0.51095E+00     179   0.62957E-04   0.92451E-03 0.14967E+01 
c  epsilon      0.32277E+04     111   0.55843E-03   0.93611E+06 0.16072E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0049084                            19
a  epsilon                 -42.248                            30
a  Local Time Step       1.652e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1087          13.575           1.554         0.37844
v  Velocity[Y]             -10.701          15.134          1.2829         0.89776
v  Velocity[Z]             -16.301          11.591         -0.9888       -0.015186
v  ǁVelocityǁ             0.020325           18.95          5.8847          7.0973
v  Pressure                 -23300      1.8748e+05      1.2382e+05           99289
v  k                    4.7114e-07           4.832        0.063777         0.10149
v  epsilon               0.0060317      1.1249e+06          1444.3          52.837
v  TurbVisc             1.1432e-12         0.49487       0.0032567        0.047361
v  CourantNb               0.11805      6.0534e+05          367.25          77.692
v  FourierNb               0.22488      2.3653e+06          218.91          3.4051
v  total_pressure        4.767e+05      6.8748e+05      6.2382e+05      5.9929e+05
v  Local Time Step            0.01         0.11635        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6437      2.7309e+06          586.16          81.097


 TIME FOR THE TIME STEP              636:        0.18283E+03

===============================================================


 INSTANT    0.637000000E+02   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         0.151048110E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888705E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000c  epsilon      0.31594E+04      91   0.33006E-03   0.35165E+06 0.10011E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0027057                            27
a  epsilon                 -29.345                            26
a  Local Time Step      1.2975e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]               -7.16           13.63          1.5427         0.37891
v  Velocity[Y]             -10.658          15.276           1.327         0.89683
v  Velocity[Z]             -18.225          9.9054        -0.99486       -0.015584
v  ǁVelocityǁ             0.013522          20.728          5.9111          7.0987
v  Pressure                 -23583      1.8758e+05      1.2387e+05           99343
v  k                    1.1275e-07          4.8299        0.063815         0.10148
v  epsilon               0.0057251      1.0932e+06          1426.9          52.848
v  TurbVisc             1.2106e-12         0.49487       0.0032537        0.047358
v  CourantNb                 0.219      7.7072e+05          368.03          77.861
v  FourierNb               0.22481      2.3653e+06           218.9           3.405
v  total_pressure       4.7642e+05 c  epsilon      0.31594E+04      91   0.33006E-03   0.35165E+06 0.10011E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0027057                            27
a  epsilon                 -29.345                            26
a  Local Time Step      1.2975e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]               -7.16           13.63          1.5427         0.37891
v  Velocity[Y]             -10.658          15.276           1.327         0.89683
v  Velocity[Z]             -18.225          9.9054        -0.99486       -0.015584
v  ǁVelocityǁ             0.013522          20.728          5.9111          7.0987
v  Pressure                 -23583      1.8758e+05      1.2387e+05           99343
v  k                    1.1275e-07          4.8299        0.063815         0.10148
v  epsilon               0.0057251      1.0932e+06          1426.9          52.848
v  TurbVisc             1.2106e-12         0.49487       0.0032537        0.047358
v  CourantNb                 0.219      7.7072e+05          368.03          77.861
v  FourierNb               0.22481      2.3653e+06           218.9           3.405
v  total_pressure       4.7642e+05      6.8758e+05      6.2387e+05      5.9934e+05
v  Local Time Step            0.01        0.062214        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6227      2.8963e+06          586.94          81.266


 TIME FOR THE TIME STEP              637:        0.17992E+03

===============================================================


 INSTANT    0.638000000E+02   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         0.745050102E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888692E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16130E+02 0.53250E+01
   Friction velocity        uet   :  0.40821E-01 0.29485E+02
   Friction velocity        uk    :  0.43168E-01 0.29485E+02
   Dimensionless distance   yplus :  0.37624E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12952
   Nb of faces within the viscous sub-layer     :      11770
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44763E+01     664   0.23851E+00   0.12092E+02 0.47486E+01 
c  Velocity[X]                                      0.27085E+01 
c  Velocity[Y]                                      0.71981E+01 
c  Velocity[Z]                                      0.21854E+01 
c  Pressure     0.12415E+00    1030   0.11536E-01   0.27840E-01 0.92949E-01 
c  k            0.51096E+00     154   0.63077E-04   0.80390E-03 0.13959E+01 
c  epsilon      0.32952E+04      96   0.82397E-03   0.12314E+07 0.17797E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0017354                            11
a  epsilon                 -82.166                            12
a  Local Time Step      1.8393e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0971          13.677           1.532         0.37938
v  Velocity[Y]              -10.71          14.982          1.2812         0.89774
v  Velocity[Z]             -18.404          11.343         -1.0043       -0.016641
v  ǁVelocityǁ            0.0019681          20.879          5.9083          7.0992
v  Pressure                 -24070      1.8781e+05      1.2405e+05           99474
v  k                    4.3695e-07          5.1135         0.06475         0.10145
v  epsilon               0.0066144      1.1666e+06          1517.8          53.102
v  TurbVisc             2.7908e-13         0.49487       0.0032556        0.047352
v  CourantNb                0.1133      5.4369e+05          375.47          77.967
v  FourierNb               0.22464      2.3653e+06          218.93          3.4059
v  total_pressure       4.7593e+05      6.8781e+05      6.2405e+05      5.9947e+05
v  Local Time Step            0.01        0.070523        0.010001        0.010005


  ** Computed values on cells
     ------------   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16130E+02 0.53250E+01
   Friction velocity        uet   :  0.40821E-01 0.29485E+02
   Friction velocity        uk    :  0.43168E-01 0.29485E+02
   Dimensionless distance   yplus :  0.37624E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12952
   Nb of faces within the viscous sub-layer     :      11770
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44763E+01     664   0.23851E+00   0.12092E+02 0.47486E+01 
c  Velocity[X]                                      0.27085E+01 
c  Velocity[Y]                                      0.71981E+01 
c  Velocity[Z]                                      0.21854E+01 
c  Pressure     0.12415E+00    1030   0.11536E-01   0.27840E-01 0.92949E-01 
c  k            0.51096E+00     154   0.63077E-04   0.80390E-03 0.13959E+01 
c  epsilon      0.32952E+04      96   0.82397E-03   0.12314E+07 0.17797E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for    ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16130E+02 0.53250E+01
   Friction velocity        uet   :  0.40821E-01 0.29485E+02
   Friction velocity        uk    :  0.43168E-01 0.29485E+02
   Dimensionless distance   yplus :  0.37624E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12952
   Nb of faces within the viscous sub-layer     :      11770
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44763E+01     664   0.23851E+00   0.12092E+02 0.47486E+01 
c  Velocity[X]                                      0.27085E+01 
c  Velocity[Y]                                      0.71981E+01 
c  Velocity[Z]                                      0.21854E+01 
c  Pressure     0.12415E+00    1030   0.11536E-01   0.27840E-01 0.92949E-01 
c  k            0.51096E+00     154   0.63077E-04   0.80390E-03 0.13959E+01 
c  epsilon      0.32952E+04      96   0.82397E-03   0.12314E+07 0.17797E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0017354                            11
a  epsilon                 -82.166                            12
a  Local Time Step      1.8393e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0971          13.677           1.532         0.37938
v  Velocity[Y]              -10.71          14.982          1.2812         0.89774
v  Velocity[Z]             -18.404          11.343         -1.0043       -0.016641
v  ǁVelocityǁ            0.0019681          20.879          5.9083          7.0992
v  Pressure                 -24070      1.8781e+05      1.2405e+05           99474
v  k                    4.3695e-07          5.1135         0.06475         0.10145
v  epsilon               0.0066144      1.1666e+06          1517.8          53.102
v  TurbVisc             2.7908e-13         0.49487       0.0032556        0.047352
v  CourantNb                0.1133      5.4369e+05          375.47          77.967
v  FourierNb               0.22464      
  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5981      2.8347e+06          591.49          81.239


 TIME FOR THE TIME STEP              640:        0.18241E+03

===============================================================


 INSTANT    0.641000000E+02   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         0.268606077E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888722E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16339E+02 0.52667E+01
   Friction velocity        uet   :  0.41011E-01 0.56454E+02
   Friction velocity        uk    :  0.40995E-01 0.56454E+02
   Dimensionless distance   yplus :  0.27294E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12957
   Nb of faces within the viscous sub-layer     :      11786
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44780E+01     647   0.23975E+00   0.91608E+01 0.41323E+01 
c  Velocity[X]                                      0.22594E+01 
c  Velocity[Y]                                      0.49030E+01 
c  Velocity[Z]                                      0.19985E+01 
c  Pressure     0.11824E+00     978   0.10780E-01   0.26464E-01 0.68545E-01 
c  k            0.51091E+00     154   0.73040E-04   0.83005E-03 0.14185E+01 
c  epsilon      0.31691E+04      94   0.96202E-03   0.99539E+06 0.16809E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  ----------
  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5981      2.8347e+06          591.49          81.239


 TIME FOR THE TIME STEP              640:        0.17671E+03

===============================================================


 INSTANT    0.641000000E+02   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         0.268606077E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888722E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maxim
  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5981      2.8347e+06          591.49          81.239


 TIME FOR THE TIME STEP              640:        0.18109E+03

===============================================================


 INSTANT    0.641000000E+02   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         0.268606077E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888722E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16339E+02 0.52667E+01
   Friction velocity        uet   :  0.41011E-01 0.56454E+02
   Friction velocity        uk    :  0.40995E-01 0.56454E+02
   Dimensionless distance   yplus :  0.27294E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12957
   Nb of faces within the viscous sub-layer     :      11786
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44780E+01     647   0.23975E+00   0.91608E+01 0.41323E+01 
c  Velocity[X]                                      0.22594E+01 
c  Velocity[Y]                                      0.49030E+01 
c  Velocity[Z]                                      0.19985E+01 
c  Pressure     0.11824E+00     978   0.10780E-01   0.26464E-01 0.68545E-01 
c  k            0.51091E+00     154   0.73040E-04   0.83005E-03 0.14185E+01 
c  epsilon      0.31691E+04      94   0.96202E-03   0.99539E+06 0.16809E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00086505                            17
a  epsilon                 -66.184                            32
a  Local Time Step      1.2913e-08                        281779


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0156          13.616          1.5427         0.37911
v  Velocity[Y]              -10.75          15.538          1.2885         0.89604
v  Velocity[Z]             -16.641          10.098        -0.99691       -0.016421
v  ǁVelocityǁ            0.0049772          19.229          5.9166           7.102
v  Pressure                 -24356      1.8805e+05      1.2421e+05           99603
v  k                    4.1966e-07          4.8224        0.063897         0.10143
v  epsilon              0.00059186      1.0909e+06          1431.9          52.902
v  TurbVisc             9.1452e-13         0.49487       0.0032571        0.047344
v  CourantNb                0.3069      7.7443e+05          369.28          77.956
v  FourierNb               0.22464      2.3653e+06          218.91          3.4061
v  total_pressure       4.7564e+05      6.8805e+05      6.2421e+05       5.996e+05
v  Local Time Step            0.01        0.085333        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6043         2.9e+06          588.19          81.362


 TIME FOR THE TIME STEP              641:        0.18346E+03

===============================================================


 INSTANT    0.642000000E+02   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        -0.269235080E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888705E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                           -  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0010569                            12
a  epsilon                 -27.386                            33
a  Local Time Step      1.7508e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2669          13.651          1.5307         0.37801
v  Velocity[Y]             -10.831          15.479          1.3254         0.89429
v  Velocity[Z]               -17.7          11.653         -1.0149       -0.016747
v  ǁVelocityǁ              0.01055          20.212          5.9774          7.1095
v  Pressure                 -24567      1.8804e+05      1.2419e+05           99565
v  k                    1.9868e-07          4.8265        0.065666         0.10141
v  epsilon               0.0012231      1.1238e+06          1557.4          53.236
v  TurbVisc             1.3049e-12         0.49487       0.0032588        0.047341
v  CourantNb               0.15028      5.7118e+05          372.49          77.905
v  FourierNb               0.22466      2.3653e+06          218.92          3.4056
v  total_pressure       4.7543e+05      6.8804e+05      6.2419e+05      5.9957e+05
v  Local Time Step            0.01        0.081877        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  -------------- -  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0010569                            12
a  epsilon                 -27.386                            33
a  Local Time Step      1.7508e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2669          13.651          1.5307         0.37801
v  Velocity[Y]             -10.831          15.479          1.3254         0.89429
v  Velocity[Z]               -17.7          11.653         -1.0149       -0.016747
v  ǁVelocityǁ              0.01055          20.212          5.9774          7.1095
v  Pressure                 -24567      1.8804e+05      1.2419e+05           99565
v  k                    1.9868e-07          4.8265        0.065666         0.10141
v  epsilon               0.0012231      1.1238e+06          1557.4          53.236
v  TurbVisc             1.3049e-12         0.49487       0.0032588        0.047341
v  CourantNb               0.15028      5.7118e+05          372.49          77.905
v  FourierNb               0.22466      2.3653e+06          218.92          3.4056
v  total_pressure       4.7543e+05      6.8804e+05      6.2419e+05      5.9957e+05
v  Local Time Step            0.01        0.081877        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.652      2.6968e+06          591.41           81.31


 TIME FOR THE TIME STEP              642:        0.18799E+03

===============================================================


 INSTANT    0.643000000E+02   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         0.209621589E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889095E+01
Free inlet               13           0         0.000000000E+00
Convective 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   :  0.32846E-01 0.61046E+02
   Friction velocity        uk    :  0.32467E-01 0.61046E+02
   Dimensionless distance   yplus :  0.28292E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12915
   Nb of faces within the viscous sub-layer     :      11733
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44791E+01     639   0.23959E+00   0.10665E+02 0.44570E+01 
c  Velocity[X]                                      0.31409E+01 
c  Velocity[Y]                                      0.56108E+01 
c  Velocity[Z]                                      0.19129E+01 
c  Pressure     0.12871E+00     962   0.11208E-01   0.28802E-01 0.58220E-01 
c  k            0.51102E+00     161   0.56924E-04   0.76941E-03 0.13653E+01 
c  epsilon      0.33180E+04     106   0.41727E-03   0.57554E+06 0.12194E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0019043                            83
a  epsilon                 -61.984                           156
a  Local Time Step      1.2271e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3035          13.604          1.5616         0.37524
v  Velocity[Y]             -10.796          15.169          1.2878         0.89446
v  Velocity[Z]             -15.549          10.165        -0.96938       -0.017673
v  ǁVelocityǁ             0.019044          18.179          5.8992          7.1068
v  Pressure                 -24924      1.8824e+05      1.2419e+05           99535
v  k                    9.6626e-08          4.9566         0.06473         0.10147
v  epsilon              0.00062941      1.2018e+06            1503          53.155
v  TurbVisc             1.3012e-12         0.49487       0.0032656        0.047339
v  CourantNb              0.030795      8.1493e+05          376.19          77.933
v  FourierNb               0.22465      2.3653e+06          218.95          3.4054
v  total_pressure       4.7508e+05      6.8824e+05      6.2419e+05      5.9953e+05
v  Local Time Step            0.01        0.076708        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6589      2.9405e+06          595.13          81.339


 TIME FOR THE TIME STE   Friction velocity        uet   :  0.32846E-01 0.61046E+02
   Friction velocity        uk    :  0.32467E-01 0.61046E+02
   Dimensionless distance   yplus :  0.28292E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12915
   Nb of faces within the viscous sub-layer     :      11733
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44791E+01     639   0.23959E+00   0.10665E+02 0.44570E+01 
c  Velocity[X]                                      0.31409E+01 
c  Velocity[Y]                                      0.56108E+01 
c  Velocity[Z]                                      0.19129E+01 
c  Pressure     0.12871E+00     962   0.11208E-01   0.28802E-01 0.58220E-01 
c  k            0.51102E+00     161   0.56924E-04   0.76941E-03 0.13653E+01 
c  epsilon      0.33180E+04     106   0.41727E-03   0.57554E+06 0.12194E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0019043                            83
a  epsilon     Friction velocity        uet   :  0.32846E-01 0.61046E+02
   Friction velocity        uk    :  0.32467E-01 0.61046E+02
   Dimensionless distance   yplus :  0.28292E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12915
   Nb of faces within the viscous sub-layer     :      11733
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44791E+01     639   0.23959E+00   0.10665E+02 0.44570E+01 
c  Velocity[X]                                      0.31409E+01 
c  Velocity[Y]                                      0.56108E+01 
c  Velocity[Z]                                      0.19129E+01 
c  Pressure     0.12871E+00     962   0.11208E-01   0.28802E-01 0.58220E-01 
c  k            0.51102E+00     161   0.56924E-04   0.76941E-03 0.13653E+01 
c  epsilon      0.33180E+04     106   0.41727E-03   0.57554E+06 0.12194E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0019043                            83
a  epsilon                 -61.984                           156
a  Local Time Step      1.2271e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3035          13.604          1.5616         0.37524
v  Velocity[Y]             -10.796          15.169          1.2878         0.89446
v  Velocity[Z]             -15.549          10.165        -0.96938       -0.017673
v  ǁVelocityǁ             0.019044          18.179          5.8992          7.1068
v  Pressure                 -24924      1.8824e+05      1.2419e+05           99535
v  k                    9.6626e-08          4.9566         0.06473         0.10147
v  epsilon              0.00062941      1.2018e+06            1503          53.155
v  TurbVisc             1.3012e-12         0.49487       0.0032656        0.047339
v  CourantNb              0.030795      8.1493e+05          376.19          77.933
v  FourierNb               0.22465      2.3653e+06          218.95          3.4054
v  total_pressure       4.7508e+05      6.8824e+05      6.2419e+05      5.9953e+05
v  Local Time Step            0.01        0.076708        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum        TIME FOR THE TIME STEP              645:        0.18879E+03

===============================================================


 INSTANT    0.646000000E+02   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         0.128902267E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889082E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15787E+02 0.52672E+01
   Friction velocity        uet   :  0.26585E-01 0.39833E+02
   Friction velocity        uk    :  0.44076E-01 0.39833E+02
   Dimensionless distance   yplus :  0.46277E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12993
   Nb of faces within the viscous sub-layer     :      11781
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44817E+01     623   0.23694E+00   0.12273E+02 0.47775E+01 
c  Velocity[X]                                      0.32735E+01 
c  Velocity[Y]                                      0.71965E+01 
c  Velocity[Z]                                      0.18033E+01 
c  Pressure     0.11825E+00    1017   0.99101E-02   0.26402E-01 0.80111E-01 
c  k            0.51113E+00     166   0.89066E-04   0.11230E-02 0.16488E+01 
c  epsilon      0.32321E+04     100   0.13283E-02   0.23026E+07 0.24332E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00038976                             7
a  epsilon                 -21.866                             7
a  Local Time Step      1.8723e-08                        281784


  ** Computed fields on cells
     ------------------------

   fie TIME FOR THE TIME STEP              645:        0.18598E+03

===============================================================


 INSTANT    0.646000000E+02   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         0.128902267E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889082E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15787E+02 0.52672E+01
   Friction velocity        uet   :  0.26585E-01 0.39833E+02
   Friction velocity        uk    :  0.44076E-01 0.39833E+02
   Dimensionless distance   yplus :  0.46277E-02 0.23857E+02
   -- TIME FOR THE TIME STEP              645:        0.18561E+03

===============================================================


 INSTANT    0.646000000E+02   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         0.128902267E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889082E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15787E+02 0.52672E+01
   Friction velocity        uet   :  0.26585E-01 0.39833E+02
   Friction velocity        uk    :  0.44076E-01 0.39833E+02
   Dimensionless distance   yplus :  0.46277E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12993
   Nb of faces within the viscous sub-layer     :      11781
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44817E+01     623   0.23694E+00   0.12273E+02 0.47775E+01 
c  Velocity[X]                                      0.32735E+01 
c  Velocity[Y]                                      0.71965E+01 
c  Velocity[Z]                                      0.18033E+01 
c  Pressure     0.11825E+00    1017   0.99101E-02   0.26402E-01 0.80111E-01 
c  k            0.51113E+00     166   0.89066E-04   0.11230E-02 0.16488E+01 
c  epsilon      0.32321E+04     100   0.13283E-02   0.23026E+07 0.24332E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00038976                             7
a  epsilon                 -21.866                             7
a  Local Time Step      1.8723e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3074          13.537          1.5277         0.37446
v  Velocity[Y]              -10.95          15.328          1.3337          0.8915
v  Velocity[Z]             -16.549          9.4688         -1.0135       -0.017095
v  ǁVelocityǁ             0.019751          19.078          5.9802           7.112
v  Pressure                 -25406      1.8821e+05        1.24e+05           99363
v  k                    4.9443e-07          4.8604        0.066056         0.10167
v  epsilon               0.0059199      1.1245e+06          1553.6          53.635
v  TurbVisc             1.2985e-12         0.49487       0.0032592        0.047355
v  CourantNb               0.13994       5.341e+05          374.06          78.014
v  FourierNb               0.22507      2.3653e+06          218.91          3.4063
v  total_pressure       4.7459e+05      6.8821e+05        6.24e+05      5.9936e+05
v  Local Time Step            0.01        0.092817        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6569      2.6597e+06          592.97           81.42


 TIME FOR THE TIME STEP              646:        0.19076E+03

===============================================================


 INSTANT    0.647000000E+02   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         0.121680440E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889084E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15659E+02 0.53009E+01
   Friction velocity        uet   :  0.38020E-01 0.42340E+02
   Friction velocity        uk    :  0.37278E-01 0.42340E+02
   Dimensionless distance   yplus :  0.34066E-02 0.23856E+
   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1128          13.653          1.5329         0.37397
v  Velocity[Y]              -10.73          15.319          1.3178         0.89209
v  Velocity[Z]             -18.091          10.119         -1.0115       -0.017771
v  ǁVelocityǁ              0.01939          20.553          5.9685          7.1054
v  Pressure                 -25647      1.8829e+05      1.2398e+05           99336
v  k                    1.7872e-08          5.0088         0.06543         0.10179
v  epsilon               0.0056663      1.1223e+06          1522.9          53.685
v  TurbVisc             1.3056e-12         0.49487       0.0032612        0.047368
v  CourantNb              0.053375       7.113e+05          378.59          78.168
v  FourierNb               0.22551      2.3653e+06          218.93          3.4052
v  total_pressure       4.7435e+05      6.8829e+05      6.2398e+05      5.9934e+05
v  Local Time Step            0.01          0.1021        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6083      2.8369e+06          597.52          81.574


 TIME FOR THE TIME STEP              647:        0.18044E+03

===============================================================


 INSTANT    0.648000000E+02   TIME STEP NUMBER             648
 ===========
   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1128          13.653          1.5329         0.37397
v  Velocity[Y]              -10.73          15.319          1.3178         0.89209
v  Velocity[Z]             -18.091          10.119         -1.0115       -0.017771
v  ǁVelocityǁ              0.01939          20.553          5.9685          7.1054
v  Pressure                 -25647      1.8829e+05      1.2398e+05           99336
v  k                    1.7872e-08          5.0088         0.06543         0.10179
v  epsilon               0.0056663      1.1223e+06          1522.9          53.685
v  TurbVisc             1.3056e-12         0.49487       0.0032612        0.047368
v  CourantNb              0.053375       7.113e+05          378.59          78.168
v  FourierNb               0.22551      2.3653e+06          218.93          3.4052
v  total_pressure       4.7435e+05      6.8829e+05      6.2398e+05      5.9934e+05
v  Local Time Step            0.01          0.1021        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6083      2.8369e+06          597.52          81.574


 TIME FOR THE TIME STEP              647:        0.17869E+03

===============================================================


 INSTANT    0.648000000E+02   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        -0.121604905E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889075E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15516E+02 0.53986E+01
   Friction velocity        uet   :  0.30755E-01 0.56603E+02
   Friction velocity        uk    :  0.34924E-01 0.56603E+02
   Dimensionless distance   ypl   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44838E+01     631   0.24075E+00   0.84978E+01 0.39770E+01 
c  Velocity[X]                                      0.22418E+01 
c  Velocity[Y]                                      0.41459E+01 
c  Velocity[Z]                                      0.21100E+01 
c  Pressure     0.10540E+00     808   0.87476E-02   0.23455E-01 0.26119E-01 
c  k            0.51122E+00     172   0.74660E-04   0.96871E-03 0.15312E+01 
c  epsilon      0.32151E+04     100   0.97121E-03   0.16521E+07 0.21287E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0080289                            11
a  epsilon                 -71.922                            27
a  Local Time Step      1.6783e-08                        281786


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0426          13.574          1.5441         0.37621
v  Velocity[Y]             -10.868          15.545          1.2784         0.89384
v  Velocity[Z]             -15.842          9.7672         -1.0059       -0.015767
v  ǁVelocityǁ             0.020186           18.43           5.957          7.1086
v  Pressure                 -25971      1.8831e+05      1.2387e+05           99247
v  k                    4.9142e-07          4.8653        0.064484          0.1019
v  epsilon               0.0042327      1.0942e+06          1467.6          53.478
v  TurbVisc             1.1762e-12         0.49487       0.0032707        0.047396
v  CourantNb               0.16894      5.9585e+05          371.79          78.015
v  FourierNb               0.22648      2.3653e+06          218.93          3.4086
v  total_pressure       4.7403e+05      6.8831e+05      6.2387e+05      5.9925e+05
v  Local Time Step            0.01         0.12354        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5812      2.7214e+06          590.72          81.424


 TIME FOR THE TIME STEP              649:        0.17441E+03

===============================================================


 INSTANT    0.650000000E+02   TIME STEP NUMBER             650
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44838E+01     631   0.24075E+00   0.84978E+01 0.39770E+01 
c  Velocity[X]                                      0.22418E+01 
c  Velocity[Y]                                      0.41459E+01 
c  Velocity[Z]                                      0.21100E+01 
c  Pressure     0.10540E+00     808   0.87476E-02   0.23455E-01 0.26119E-01 
c  k            0.51122E+00     172   0.74660E-04   0.96871E-03 0.15312E+01 
c  epsilon      0.32151E+04     100   0.97121E-03   0.16521E+07 0.21287E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0080289                            11
a  epsilon                 -71.922                            27
a  Local Time Step      1.6783e-08                        281786


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]     Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44838E+01     631   0.24075E+00   0.84978E+01 0.39770E+01 
c  Velocity[X]                                      0.22418E+01 
c  Velocity[Y]                                      0.41459E+01 
c  Velocity[Z]                                      0.21100E+01 
c  Pressure     0.10540E+00     808   0.87476E-02   0.23455E-01 0.26119E-01 
c  k            0.51122E+00     172   0.74660E-04   0.96871E-03 0.15312E+01 
c  epsilon      0.32151E+04     100   0.97121E-03   0.16521E+07 0.21287E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0080289                            11
a  epsilon                 -71.922                            27
a  Local Time Step      1.6783e-08                        281786


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0426          13.574          1.5441         0.37621
v  Velocity[Y]             -10.868          15.545          1.2784         0.89384
v  Velocity[Z]             -15.842          9.7672         -1.0059       -0.015767
v  ǁVelocityǁ             0.020186           18.43           5.957          7.1086
v  Pressure                 -25971      1.8831e+05      1.2387e+05           99247
v  k                    4.9142e-07          4.8653        0.064484          0.1019
v  epsilon               0.0042327      1.0942e+06          1467.6          53.478
v  TurbVisc             1.1762e-12         0.49487       0.0032707        0.047396
v  CourantNb               0.16894      5.9585e+05          371.79          78.015
v  FourierNb               0.22648      2.3653e+06          218.93          3.4086
v  total_pressure       4.7403e+05      6.8831e+05      6.2387e+05      5.9925e+05
v  Local Time Step            0.01         0.12354        0.010001        0.010008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5812      2.7214e+06          590.72          81.424


 TIME FOR THE TIME STEP              649:        0.17761E+03

==============================================================---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.140525947E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889074E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15583E+02 0.52803E+01
   Friction velocity        uet   :  0.38876E-01 0.59066E+02
   Friction velocity        uk    :  0.44572E-01 0.59066E+02
   Dimensionless distance   yplus :  0.40098E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13017
   Nb of faces within the viscous sub-layer     :      11665
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44849E+01     636   0.24157E+00   0.10391E+02 0.43968E+01 
c  Velocity[X]                                      0.27021E+01 
c  Velocity[Y]                                      0.50981E+01 
c  Velocity[Z]                                      0.25909E+01 
c  Pressure     0.11034E+00     862   0.90668E-02   0.24481E-01 0.43135E-01 
c  k            0.51126E+00     161   0.82383E-04   0.96199E-03 0.15258E+01 
c  epsilon      0.32860E+04      98   0.96500E-03   0.13959E+07 0.18793E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.002297                            32
a  epsilon                 -15.732                            65
a  Local Time Step      1.2216e-08                        281786


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1728          13.682          1.5392          0.3758
v  Velocity[Y]             -10.827          15.515          1.3192         0.89303
v  Veloc---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.140525947E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889074E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15583E+02 0.52803E+01
   Friction velocity        uet   :  0.38876E-01 0.59066E+02
   Friction velocity        uk    :  0.44572E-01 0.59066E+02
   Dimensionless distance   yplus :  0.40098E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13017
   Nb of faces within the viscous sub-layer     :      11665
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
 ---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.140525947E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889074E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15583E+02 0.52803E+01
   Friction velocity        uet   :  0.38876E-01 0.59066E+02
   Friction velocity        uk    :  0.44572E-01 0.59066E+02
   Dimensionless distance   yplus :  0.40098E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13017
   Nb of faces within the viscous sub-layer     :      11665
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44849E+01     636   0.24157E+00   0.10391E+02 0.43968E+01 
c  Velocity[X]                                      0.27021E+01 
c  Velocity[Y]                                      0.50981E+01 
c  Velocity[Z]                                      0.25909E+01 
c  Pressure     0.11034E+00     862   0.90668E-02   0.24481E-01 0.43135E-01 
c  k            0.51126E+00     161   0.82383E-04   0.96199E-03 0.15258E+01 
c  epsilon      0.32860E+04      98   0.96500E-03   0.13959E+07 0.18793E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.002297                            32
a  epsilon                 -15.732                            65
a  Local Time Step      1.2216e-08                        281786


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  ---v  Velocity[Z]             -18.401          10.175        -0.98526       -0.015843
v  ǁVelocityǁ             0.036573          20.908          5.9413          7.1086
v  Pressure                 -26215      1.8859e+05      1.2394e+05           99289
v  k                    4.3216e-07          5.6662        0.065738         0.10184
v  epsilon               0.0013528      1.3665e+06          1572.8          53.743
v  TurbVisc             1.1955e-12         0.49487       0.0032721        0.047394
v  CourantNb              0.049133      7.2026e+05          380.32          78.155
v  FourierNb               0.22669      2.3653e+06          218.94          3.4077
v  total_pressure       4.7379e+05      6.8859e+05      6.2394e+05      5.9929e+05
v  Local Time Step            0.01        0.093071        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5803      2.8458e+06          599.25          81.563


 TIME FOR THE TIME STEP              652:        0.17870E+03

===============================================================


 INSTANT    0.653000000E+02   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         0.171219436E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888703E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15809E+02 0.52668E+01
   Friction velocity        uet   :  0.36886E-01 0.36710E+02
   Friction velocity        uk    :  0.40394E-01 0.36710E+02
   Dimensionless distance   yplus :  0.46842E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13037
   Nb of faces within the viscous sub-layer     :      11723
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-------------v  Velocity[Z]             -18.401          10.175        -0.98526       -0.015843
v  ǁVelocityǁ             0.036573          20.908          5.9413          7.1086
v  Pressure                 -26215      1.8859e+05      1.2394e+05           99289
v  k                    4.3216e-07          5.6662        0.065738         0.10184
v  epsilon               0.0013528      1.3665e+06          1572.8          53.743
v  TurbVisc             1.1955e-12         0.49487       0.0032721        0.047394
v  CourantNb              0.049133      7.2026e+05          380.32          78.155
v  FourierNb               0.22669      2.3653e+06          218.94          3.4077
v  total_pressure       4.7379e+05      6.8859e+05      6.2394e+05      5.9929e+05
v  Local Time Step            0.01        0.093071        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5803      2.8458e+06          599.25          81.563


 TIME FOR THE TIME STEP              652:        0.17622E+03

===============================================================


 INSTANT    0.653000000E+02   TIME STEP NUMBER             653
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet         v  Velocity[Z]             -18.401          10.175        -0.98526       -0.015843
v  ǁVelocityǁ             0.036573          20.908          5.9413          7.1086
v  Pressure                 -26215      1.8859e+05      1.2394e+05           99289
v  k                    4.3216e-07          5.6662        0.065738         0.10184
v  epsilon               0.0013528      1.3665e+06          1572.8          53.743
v  TurbVisc             1.1955e-12         0.49487       0.0032721        0.047394
v  CourantNb              0.049133      7.2026e+05          380.32          78.155
v  FourierNb               0.22669      2.3653e+06          218.94          3.4077
v  total_pressure       4.7379e+05      6.8859e+05      6.2394e+05      5.9929e+05
v  Local Time Step            0.01        0.093071        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5803      2.8458e+06          599.25          81.563


 TIME FOR THE TIME STEP              652:        0.18375E+03

===============================================================


 INSTANT    0.653000000E+02   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         0.171219436E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888703E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15809E+02 0.52668E+01
   Friction velocity        uet   :  0.36886E-01 0.36710E+02
   Friction velocity        uk    :  0.40394E-01 0.36710E+02
   Dimensionless distance   yplus :  0.46842E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13037
   Nb of faces within the viscous sub-layer     :      11723
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44817E+01     591   0.23658E+00   0.90058E+01 0.40940E+01 
c  Velocity[X]                                      0.28178E+01 
c  Velocity[Y]                                      0.39432E+01 
c  Velocity[Z]                                      0.22448E+01 
c  Pressure     0.10843E+00     778   0.86214E-02   0.24041E-01 0.32909E-01 
c  k            0.51126E+00     163   0.70174E-04   0.94336E-03 0.15109E+01 
c  epsilon      0.32533E+04     100   0.85813E-03   0.15626E+07 0.20490E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00076935                             5
a  epsilon                 -56.758                            14
a  Local Time Step      1.7948e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1745          13.594          1.5432         0.37662
v  Velocity[Y]             -10.802          15.696          1.2951         0.89421
v  Velocity[Z]             -14.952          10.575         -1.0148       -0.015016
v  ǁVelocityǁ             0.031195          18.518          5.9666          7.1101
v  Pressure                 -26233      1.8865e+05      1.2395e+05           99319
v  k                    4.6257e-07          4.8867        0.064999         0.10183
v  epsilon               0.0068575      1.1032e+06          1486.5          53.679
v  TurbVisc             1.2386e-12         0.49487        0.003278        0.047388
v  CourantNb               0.15963      5.5717e+05          374.47          78.051
v  FourierNb               0.22644      2.3653e+06          218.95          3.4061
v  total_pressure       4.7377e+05      6.8865e+05      6.2395e+05      5.9932e+05
v  Local Time Step            0.01        0.070811        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4682      2.6828e+06          593.42          81.457


 TIME FOR THE TIME STEP              653:        0.17143E+03

===============================================================


 INSTANT    0.654000000E+02   TIME STEP NUMBER             654
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
-----------------------------------------------------------------------------
c  Velocity     0.44838E+01     598   0.23864E+00   0.11766E+02 0.46767E+01 
c  Velocity[X]                                      0.28477E+01 
c  Velocity[Y]                                      0.68200E+01 
c  Velocity[Z]                                      0.20979E+01 
c  Pressure     0.10587E+00     940   0.83931E-02   0.23461E-01 0.43841E-01 
c  k            0.51131E+00     170   0.63668E-04   0.78184E-03 0.13753E+01 
c  epsilon      0.32439E+04      98   0.65581E-03   0.68444E+06 0.13470E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0013969                            26
a  epsilon                 -57.482                            41
a  Local Time Step       1.378e-08                        281786


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]               -7.33          13.531          1.5359         0.37496
v  Velocity[Y]             -10.857          15.304          1.3427         0.89284
v  Velocity[Z]             -17.103          11.055         -1.0249       -0.015059
v  ǁVelocityǁ             0.031549          19.678          5.9967          7.1137
v  Pressure                 ------------------------------------------------------------------------------
c  Velocity     0.44838E+01     598   0.23864E+00   0.11766E+02 0.46767E+01 
c  Velocity[X]                                      0.28477E+01 
c  Velocity[Y]                                      0.68200E+01 
c  Velocity[Z]                                      0.20979E+01 
c  Pressure     0.10587E+00     940   0.83931E-02   0.23461E-01 0.43841E-01 
c  k            0.51131E+00     170   0.63668E-04   0.78184E-03 0.13753E+01 
c  epsilon      0.32439E+04      98   0.65581E-03   0.68444E+06 0.13470E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0013969                            26
a  epsilon                 -57.482                            41
a  Local Time Step       1.378e-08                        281786


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]               -7.33          13.531          1.5359         0.37496
v  Velocity[Y]             -10.857          15.304          1.3427         0.89284
v  Velocity[Z]             -17.103          11.055         -1.0249       -0.015059
v  ǁVelocityǁ             0.031549          19.678          5.9967          7.1137
v  Pressure                 -26366      1.8865e+05       1.239e+05           99280
v  k                    5.2366e-08          4.8139        0.065721         0.10185
v  epsilon               0.0060313      1.1211e+06          1517.1          53.797
v  TurbVisc             1.3288e-12         0.49487       0.0032688        0.047383
v  CourantNb              0.044961      7.2568e+05          375.93          78.191
v  FourierNb               0.22633      2.3653e+06          218.92          3.4065
v  total_pressure       4.7363e+05      6.8865e+05       6.239e+05      5.9928e+05
v  Local Time Step            0.01        0.056143            0.01        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6405      2.8513e+06          594.85          81.598


 TIME FOR THE TIME STEP              654:        0.18116E+03

===============================================================


 INSTANT    0.655000000E+02   TIME STEP NUMBER             655
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
----------------------------------------------Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888714E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15939E+02 0.54131E+01
   Friction velocity        uet   :  0.20183E-01 0.41617E+02
   Friction velocity        uk    :  0.20145E-01 0.41617E+02
   Dimensionless distance   yplus :  0.51829E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13016
   Nb of faces within the viscous sub-layer     :      11670
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44924E+01     657   0.23879E+00   0.10827E+02 0.44871E+01 
c  Velocity[X]                                      0.31008E+01 
c  Velocity[Y]                                      0.57242E+01 
c  Velocity[Z]                                      0.20019E+01 
c  Pressure     0.10979E+00     829   0.85878E-02   0.24293E-01 0.39788E-01 
c  k            0.51141E+00     163   0.71174E-04   0.10747E-02 0.16119E+01 
c  epsilon      0.33987E+04      93   0.11629E-02   0.15785E+07 0.19489E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0022054                            15
a  epsilon                 -81.608                            42
a  Local Time Step      1.6901e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3365          13.705          1.5468         0.37426
v  Velocity[Y]             -10.828          15.268           1.287         0.89427
v  Velocity[Z]             -17.184          10.806        -0.99346       -0.015012
v  ǁVelocityǁ             0.029798          19.734          5.9564          7.1105
v  Pressure                 -26503      1.8883e+05      1.2395e+05           99339
v  k                    3.8011e-07          5.0846        0.066116         0.10198
v  epsilon              0.00022816      1.2157e+06    Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888714E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15939E+02 0.54131E+01
   Friction velocity        uet   :  0.20183E-01 0.41617E+02
   Friction velocity        uk    :  0.20145E-01 0.41617E+02
   Dimensionless distance   yplus :  0.51829E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13016
   Nb of faces within the viscous sub-layer     :      11670
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44924E+01     657   0.23879E+00   0.10827E+02 0.44871E+01 
c  Velocity[X]                       Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888714E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15939E+02 0.54131E+01
   Friction velocity        uet   :  0.20183E-01 0.41617E+02
   Friction velocity        uk    :  0.20145E-01 0.41617E+02
   Dimensionless distance   yplus :  0.51829E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13016
   Nb of faces within the viscous sub-layer     :      11670
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44924E+01     657   0.23879E+00   0.10827E+02 0.44871E+01 
c  Velocity[X]                                      0.31008E+01 
c  Velocity[Y]                                      0.57242E+01 
c  Velocity[Z]                                      0.20019E+01 
c  Pressure     0.10979E+00     829   0.85878E-02   0.24293E-01 0.39788E-01 
c  k            0.51141E+00     163   0.71174E-04   0.10747E-02 0.16119E+01 
c  epsilon      0.33987E+04      93   0.11629E-02   0.15785E+07 0.19489E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0022054                            15
a  epsilon                 -81.608                            42
a  Local Time Step      1.6901e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3365          13.705          1.5468         0.37426
v  Velocity[Y]             -10.828          15.268           1.287         0.89427
v  Velocity[Z]             -17.184          10.806        -0.99346       -0.015012
v  ǁVelocityǁ             0.029798     v  epsilon               0.0073596      1.1262e+06          1502.6          53.885
v  TurbVisc             1.3949e-12         0.49487        0.003283        0.047407
v  CourantNb              0.016377      5.9343e+05           376.1          78.085
v  FourierNb                 0.227      2.3653e+06          218.93          3.4067
v  total_pressure       4.7347e+05      6.8883e+05      6.2392e+05      5.9933e+05
v  Local Time Step            0.01        0.074726        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6016       2.719e+06          595.03          81.492


 TIME FOR THE TIME STEP              657:        0.16986E+03

===============================================================


 INSTANT    0.658000000E+02   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        -0.184931129E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889077E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15962E+02 0.52952E+01
   Friction velocity        uet   :  0.35904E-01 0.54826E+02
   Friction velocity        uk    :  0.43539E-01 0.54826E+02
   Dimensionless distance   yplus :  0.45114E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13004
   Nb of faces within the viscous sub-layer     :      11674
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44877E+01     594   0.24223E+00   0.10605E+02 0.44399E+01 
c  Velocity[X]                                      0.24677E+01 
c  Velocity[Y]                                      0.58597E+01 
c  Velocity[Z]                                      0.22774E+0v  epsilon               0.0073596      1.1262e+06          1502.6          53.885
v  TurbVisc             1.3949e-12         0.49487        0.003283        0.047407
v  CourantNb              0.016377      5.9343e+05           376.1          78.085
v  FourierNb                 0.227      2.3653e+06          218.93          3.4067
v  total_pressure       4.7347e+05      6.8883e+05      6.2392e+05      5.9933e+05
v  Local Time Step            0.01        0.074726        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6016       2.719e+06          595.03          81.492


 TIME FOR THE TIME STEP              657:        0.18595E+03

===============================================================


 INSTANT    0.658000000E+02   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        -0.184931129E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889077E+01
Free inlet               13 v  epsilon               0.0073596      1.1262e+06          1502.6          53.885
v  TurbVisc             1.3949e-12         0.49487        0.003283        0.047407
v  CourantNb              0.016377      5.9343e+05           376.1          78.085
v  FourierNb                 0.227      2.3653e+06          218.93          3.4067
v  total_pressure       4.7347e+05      6.8883e+05      6.2392e+05      5.9933e+05
v  Local Time Step            0.01        0.074726        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6016       2.719e+06          595.03          81.492


 TIME FOR THE TIME STEP              657:        0.17087E+03

===============================================================


 INSTANT    0.658000000E+02   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        -0.184931129E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889077E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15962E+02 0.52952E+01
   Friction velocity        uet   :  0.35904E-01 0.54826E+02
   Friction velocity        uk    :  0.43539E-01 0.54826E+02
   Dimensionless distance   yplus :  0.45114E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13004
   Nb of faces within the viscous sub-layer     :      11674
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44877E+01     594   0.24223E+00   0.10605E+02 0.44399E+01 
c  Velocity[X]                                      0.24677E+01 
c  Velocity[Y]                                      0.58597E+01 
c  Velocity[Z]                                      0.22774E+01 
c  Pressure     0.10785E+00     924   0.84065E-02   0.23829E-01 0.37343E-01 
c  k            0.51131E+00     172   0.64887E-04   0.84544E-03 0.14301E+01 
c  epsilon      0.32399E+04      98   0.49018E-03   0.59586E+06 0.12626E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0006848                            32
a  epsilon                 -20.965                            47
a  Local Time Step      1.2361e-08                        281786


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2052          13.667          1.5309         0.37542
v  Velocity[Y]             -10.825          15.284          1.3253         0.89292
v  Velocity[Z]             -15.807          9.7582         -1.0248       -0.013845
v  ǁVelocityǁ            0.0088056          18.338          6.0028          7.1128
v  Pressure                 -26502      1.8893e+05      1.2397e+05           99372
v  k                    2.4199e-07          4.8444        0.065625         0.10199
v  epsilon              0.00032756      1.1384e+06          1507.5          53.898
v  TurbVisc              1.229e-12         0.49487       0.0032773        0.047411
v  CourantNb              0.068053      8.0899e+05           376.3            78.2
v  FourierNb               0.22714      2.3653e+06          218.92          3.4076
v  total_pressure        4.735e+05      6.8893e+05      6.2397e+05      5.9937e+05
v  Local Time Step            0.01        0.082199        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5939      2.9346e+06          595.22          81.607


 TIME FOR THE TIME STEP              658:        0.17649E+03

===============================================================


 INSTANT    0.659000000E+02   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         0.594486906E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3  c  Velocity[Z]                                      0.21897E+01 
c  Pressure     0.10775E+00    1009   0.85566E-02   0.23783E-01 0.71071E-01 
c  k            0.51133E+00     173   0.11786E-03   0.15613E-02 0.19433E+01 
c  epsilon      0.33373E+04     108   0.16262E-02   0.40839E+07 0.30870E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00092416                             8
a  epsilon                 -39.065                            25
a  Local Time Step      1.3271e-08                        281780


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1976          13.716          1.5408         0.37511
v  Velocity[Y]             -10.864          15.947           1.329         0.89296
v  Velocity[Z]              -16.83          10.813         -1.0165       -0.014383
v  ǁVelocityǁ             0.014798          19.378          6.0297          7.1138
v  Pressure                 -26460      1.8907e+05      1.2407e+05           99446
v  k                    4.3756e-07          4.9813        0.066927           0.102
v  epsilon              0.00023732      1.1123e+06          1619.4          54.378
v  TurbVisc             1.3541e-12         0.49487       0.003281c  Velocity[Z]                                      0.21897E+01 
c  Pressure     0.10775E+00    1009   0.85566E-02   0.23783E-01 0.71071E-01 
c  k            0.51133E+00     173   0.11786E-03   0.15613E-02 0.19433E+01 
c  epsilon      0.33373E+04     108   0.16262E-02   0.40839E+07 0.30870E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00092416                             8
a  epsilon                 -39.065                            25
a  Local Time Step      1.3271e-08                        281780


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1976          13.716          1.5408         0.37511
v  Velocity[Y]             -10.864          15.947           1.329         0.89296
v  Velocity[Z]              -16.83          10.813         -1.0165       -0.014383
v  ǁVelocityǁ             0.014798          19.378          6.0297          7.1138
v  Pressure                 -26460      1.8907e+05      1.2407e+05           99446
v  k                    4.3756e-07          4.9813        0.066927           0.102
v  epsilon              0.00023732      1.1123e+06          1619.4          54.378
v  TurbVisc             1.3541e-12         0.49487       0.0032813        0.047407
v  CourantNb             0.0080429      7.5355e+05          381.12          78.212
v  FourierNb               0.22702      2.3653e+06          218.92          3.4086
v  total_pressure       4.7354e+05      6.8907e+05      6.2407e+05      5.9945e+05
v  Local Time Step            0.01        0.090419        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6351      2.8791e+06          600.04          81.621


 TIME FOR THE TIME STEP              659:        0.17905E+03

===============================================================


 INSTANT    0.660000000E+02   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         0.145212463E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0       Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16075E+02 0.53171E+01
   Friction velocity        uet   :  0.34942E-01 0.27354E+02
   Friction velocity        uk    :  0.37732E-01 0.27354E+02
   Dimensionless distance   yplus :  0.16843E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13008
   Nb of faces within the viscous sub-layer     :      11610
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44859E+01     625   0.23704E+00   0.10728E+02 0.44668E+01 
c  Velocity[X]                                      0.34016E+01 
c  Velocity[Y]                                      0.51852E+01 
c  Velocity[Z]                                      0.21409E+01 
c  Pressure     0.11008E+00     871   0.84656E-02   0.24291E-01 0.38933E-01 
c  k            0.51125E+00     166   0.67964E-04   0.10103E-02 0.15634E+01 
c  epsilon      0.33256E+04     103   0.69559E-03   0.15096E+07 0.19778E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0032445                            14
a  epsilon                 -772.98                            36
a  Local Time Step      1.5215e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2708          13.575           1.557         0.37612
v  Velocity[Y]             -10.739          15.823          1.2877         0.89421
v  Velocity[Z]             -18.193          10.275         -1.0024       -0.014046
v  ǁVelocityǁ             0.007075          20.653          5.9719          7.1109
v  Pressure                 -26398      1.8918e+05      1.2409e+05           99463
v  k                    4.9777e-07           4.968        0.065666         0.10192
v  epsilon              0.00027654      1.1477e+06          1520.4          53.926
v  TurbVisc             1.2841e-12         0.49487       0.0032969        0.047399
v  CourantNb               0.42742      6.5726e+05          378.98          78.113
v  FourierNb               0.22644      2.3653e+06          2Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16075E+02 0.53171E+01
   Friction velocity        uet   :  0.34942E-01 0.27354E+02
   Friction velocity        uk    :  0.37732E-01 0.27354E+02
   Dimensionless distance   yplus :  0.16843E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13008
   Nb of faces within the viscous sub-layer     :      11610
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44859E+01     625   0.23704E+00   0.10728E+02 0.44668E+01 
c  Velocity[X]                                      0.34016E+01 
c  Velocity[Y]                                      0.51852E+01 
c  Velocity[Z]                                      0.21409E+01 
c  Pressure     0.11008E+00     871   0.84656E-02   0.24291E-01 0.38933E-01 
c  k            0.511Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16075E+02 0.53171E+01
   Friction velocity        uet   :  0.34942E-01 0.27354E+02
   Friction velocity        uk    :  0.37732E-01 0.27354E+02
   Dimensionless distance   yplus :  0.16843E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13008
   Nb of faces within the viscous sub-layer     :      11610
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44859E+01     625   0.23704E+00   0.10728E+02 0.44668E+01 
c  Velocity[X]                                      0.34016E+01 
c  Velocity[Y]                                      0.51852E+01 
c  Velocity[Z]                                      0.21409E+01 
c  Pressure     0.11008E+00     871   0.84656E-02   0.24291E-01 0.38933E-01 
c  k            0.51125E+00     166   0.67964E-04   0.10103E-02 0.15634E+01 
c  epsilon      0.33256E+04     103   0.69559E-03   0.15096E+07 0.19778E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0032445                            14
a  epsilon                 -772.98                            36
a  Local Time Step      1.5215e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2708          13.575           1.557         0.37612
v  Velocity[Y]             -10.739          15.823          1.2877         0.89421
v  Velocity[Z]             -18.193          10.275         -1.0024       -0.014046
v  ǁVelocityǁ             0.007075          20.653          5.9719          7.1109
v  Pressure                 -26398      1.8918e+05      1.2409e+05           99463
v  k                    4.9777e-07           4.968        0.065666         0.10192
v  epsilon              0.00027654     v  FourierNb               0.22627      2.3653e+06          218.94          3.4079
v  total_pressure       4.7361e+05      6.8924e+05      6.2413e+05      5.9948e+05
v  Local Time Step            0.01        0.077435        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.621      2.9432e+06          594.97          81.612


 TIME FOR THE TIME STEP              662:        0.17356E+03

===============================================================


 INSTANT    0.663000000E+02   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        -0.770042082E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888703E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15806E+02 0.52669E+01
   Friction velocity        uet   :  0.26281E-01 0.39736E+02
   Friction velocity        uk    :  0.28421E-01 0.39736E+02
   Dimensionless distance   yplus :  0.42669E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13091
   Nb of faces within the viscous sub-layer     :      11638
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44906E+01     664   0.24639E+00   0.10858E+02 0.44907E+01 
c  Velocity[X]                                      0.27853E+01 
c  Velocity[Y]                                      0.58293E+01 
c  Velocity[Z]                                      0.22430E+01 
c  Pressure     0.10828E+00     789   0.85178E-02   0.23874E-01 0.24473E-01 
c  k            0.51128E+00     184   0.90440E-04   0.11532E-02 0.16702E+01 
c  epsilon      0.33122E+04     102   0.12615E-02   0.23199E+07 0.23857E+02 
---------------v  FourierNb               0.22627      2.3653e+06          218.94          3.4079
v  total_pressure       4.7361e+05      6.8924e+05      6.2413e+05      5.9948e+05
v  Local Time Step            0.01        0.077435        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.621      2.9432e+06          594.97          81.612


 TIME FOR THE TIME STEP              662:        0.17122E+03

===============================================================


 INSTANT    0.663000000E+02   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        -0.770042082E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888703E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------v  FourierNb               0.22627      2.3653e+06          218.94          3.4079
v  total_pressure       4.7361e+05      6.8924e+05      6.2413e+05      5.9948e+05
v  Local Time Step            0.01        0.077435        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.621      2.9432e+06          594.97          81.612


 TIME FOR THE TIME STEP              662:        0.17278E+03

===============================================================


 INSTANT    0.663000000E+02   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        -0.770042082E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888703E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15806E+02 0.52669E+01
   Friction velocity        uet   :  0.26281E-01 0.39736E+02
   Friction velocity        uk    :  0.28421E-01 0.39736E+02
   Dimensionless distance   yplus :  0.42669E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13091
   Nb of faces within the viscous sub-layer     :      11638
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44906E+01     664   0.24639E+00   0.10858E+02 0.44907E+01 
c  Velocity[X]                                      0.27853E+01 
c  Velocity[Y]                                      0.58293E+01 
c  Velocity[Z]                                      0.22430E+01 
c  Pressure     0.10828E+00     789   0.85178E-02   0.23874E-01 0.24473E-01 
c  k            0.51128E+00     184   0.90440E-04   0.11532E-02 0.16702E+01 
c  epsilon      0.33122E+04     102   0.12615E-02   0.23199E+07 0.23857E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00068634                            10
a  epsilon                 -7.2899                            16
a  Local Time Step      1.4976e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3104          13.677          1.5467         0.37492
v  Velocity[Y]             -10.893          16.068          1.3339         0.89323
v  Velocity[Z]             -14.812          10.064         -1.0048       -0.014374
v  ǁVelocityǁ             0.037164           18.82          6.0291          7.1158
v  Pressure                 -26464      1.8924e+05      1.2411e+05           99476
v  k                    3.8791e-07          4.9788        0.066788          0.1019
v  epsilon               0.0056895      1.1142e+06          1599.3          54.191
v  TurbVisc             1.4276e-12         0.49487       0.0032818        0.047389
v  CourantNb               0.14062      6.6774e+05          380.38          78.241
v  FourierNb               0.22623      2.3653e+06          218.93          3.4064
v  total_pressure       4.7354e+05      6.8924e+05      6.2411e+05      5.9948e+05
v  Local Time Step            0.01        0.085179            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6008      2.7933e+06          599.31          81.648


 TIME FOR THE TIME STEP              663:        0.17401E+03

===============================================================


 INSTANT    0.664000000E+02   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         0.130925476E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889064E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
----------------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0008691                             6
a  epsilon                 -12.912                             8
a  Local Time Step      1.6678e-08                        281787


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4079          13.778          1.5439         0.37466
v  Velocity[Y]             -10.745          15.466            1.31         0.89353
v  Velocity[Z]             -15.127          11.429         -1.0049       -0.014695
v  ǁVelocityǁ             0.023929          18.303          5.9905          7.1098
v  Pressure                 -26558      1.8927e+05       1.241e+05           99470
v  k                       5.2e-07          5.3068        0.066761         0.10194
v  epsilon                0.005442      1.1774e+06          1605.3          54.168
v  TurbVisc             1.2747e-12         0.49487       0.0032812        0.047388
v  CourantNb              0.033603       5.996e+05          383.49          78.296
v  FourierNb               0.22616      2.3653e+06          218.94          3.4069
v  total_pressure       4.7344e+05      6.8927e+05       6.241e+05      5.9947e+05
v  Local Time Step           -----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0008691                             6
a  epsilon                 -12.912                             8
a  Local Time Step      1.6678e-08                        281787


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4079          13.778          1.5439         0.37466
v  Velocity[Y]             -10.745          15.466            1.31         0.89353
v  Velocity[Z]             -15.127          11.429         -1.0049       -0.014695
v  ǁVelocityǁ             0.023929          18.303          5.9905          7.1098
v  Pressure                 -26558      1.8927e+05       1.241e+05           99470
v  k                       5.2e-07          5.3068        0.066761         0.10194
v  epsilon                0.005442      1.1774e+06          1605.3          54.168
v  TurbVisc             1.2747e-12         0.49487       0.0032812        0.047388
v  CourantNb              0.033603       5.996e+05          383.49          78.296
v  FourierNb               0.22616      2.3653e+06          218.94          3.4069
v  total_pressure       4.7344e+05      6.8927e+05       6.241e+05      5.9947e+05
v  Local Time Step            0.01        0.093697            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6097      2.6903e+06          602.42          81.703


 TIME FOR THE TIME STEP              664:        0.16951E+03

===============================================================


 INSTANT    0.665000000E+02   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         0.868601772E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889058E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefi------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16200E+02 0.53141E+01
   Friction velocity        uet   :  0.39337E-01 0.53876E+02
   Friction velocity        uk    :  0.43386E-01 0.53876E+02
   Dimensionless distance   yplus :  0.42644E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13050
   Nb of faces within the viscous sub-layer     :      11641
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44920E+01     605   0.24201E+00   0.87598E+01 0.40354E+01 
c  Velocity[X]                                      0.21242E+01 
c  Velocity[Y]                                      0.44439E+01 
c  Velocity[Z]                                      0.21917E+01 
c  Pressure     0.10531E+00     920   0.79993E-02   0.23220E-01 0.45269E-01 
c  k            0.51140E+00     171   0.74880E-04   0.10198E-02 0.15701E+01 
c  epsilon      0.32403E+04     111   0.87954E-03   0.12473E+07 0.18368E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0047327                            29
a  epsilon                 -508.89                            64
a  Local Time Step      1.2481e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3672           13.62          1.5511         0.37495
v  Velocity[Y]             -10.836          15.347          1.2977         0.89372
v  Velocity[Z]             -16.021          9.6713         -1.0041       -0.013788
v  ǁVelocityǁ               0.0161          18.625          5.9958          7.1127
v  Pressure                 -26592      1.8931e+05      1.2412e+05           99498
v  k                    3.1714e-07           4.839        0.065487         0.10207
v  epsilon              0.00025283        1.14e+06          1490.5          53.965
v  TurbVisc             1.5568e-12         0.49487       0.0032791        0.047403
v  CourantNb              0.053597       8.012e+05          376.28          78.223
v  FourierNb               0.22652      2.3653e+06          218.92           3.408
v  total_pressure       4.7341e+05      6.8931e+05      6.2412e+05       5.995e+05
v  Local Time Step            0.01        0.047217            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               mi------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16200E+02 0.53141E+01
   Friction velocity        uet   :  0.39337E-01 0.53876E+02
   Friction velocity        uk    :  0.43386E-01 0.53876E+02
   Dimensionless distance   yplus :  0.42644E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13050
   Nb of faces within the viscous sub-layer     :      11641
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44920E+01     605   0.24201E+00   0.87598E+01 0.40354E+01 
c  Velocity[X]                                      0.21242E+01 
c  Velocity[Y]                                      0.44439E+01 
c  Velocity[Z]                                      0.21917E+01 
c  Pressure     0.10531E+00     920   0.79993E-02   0.23220E-01 0.45269E-01 
c  k            0.51140E+00     171   0.74880E-04   0.10198E-02 0.15701E+01 
c  epsilon      0.32403E+04     111   0.87954E-03   0.12473E+07 0.18368E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     ----------------------------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16200E+02 0.53141E+01
   Friction velocity        uet   :  0.39337E-01 0.53876E+02
   Friction velocity        uk    :  0.43386E-01 0.53876E+02
   Dimensionless distance   yplus :  0.42644E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13050
   Nb of faces within the viscous sub-layer     :      11641
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44920E+01     605   0.24201E+00   0.87598E+01 0.40354E+01 
c  Velocity[X]                                      0.21242E+01 
c  Velocity[Y]                                      0.44439E+01 
c  Velocity[Z]                                      0.21917E+01 
c  Pressure     0.10531E+00     920   0.79993E-02   0.23220E-01 0.45269E-01 
c  k            0.51140E+00     171   0.74880E-04   0.10198E-02 0.15701E+01 
c  epsilon      0.32403E+04     111   0.87954E-03   0.12473E+07 0.18368E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0047327                            29
a  epsilon                 -508.89                            64
a  Local Time Step      1.2481e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3672           13.62          1.5511         0.37495
v  Velocity[Y]             -10.836          15.347          1.2977         0.89372
v  Velocity[Z]             -16.021          9.6713         -1.0041       -0.013788
v  ǁVelocityǁ               0.0161          18.625          5.9958          7.1127
v  Pressure                 -26592      1.8931e+05      1.2412e+05           99498
v  k                    3.1714e-07           4.839        0.065487         0.10207
v  epsilon              0.00025283        1.14e+06          1490.5          53.965
v  TurbVisc             1.5568e-12         0.49487       0.0032791        0.047403
v  CourantNb              0.053597       8.012e+05          376.28          78.223
v  FourierNb               0.22652      2.3653e+06          218.92           3.408
v  total_pressure 
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6118      2.6965e+06          597.93          81.645


 TIME FOR THE TIME STEP              667:        0.18204E+03

===============================================================


 INSTANT    0.668000000E+02   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        -0.427334065E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888689E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16224E+02 0.53559E+01
   Friction velocity        uet   :  0.24350E-01 0.29218E+02
   Friction velocity        uk    :  0.41475E-01 0.29218E+02
   Dimensionless distance   yplus :  0.24308E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13046
   Nb of faces within the viscous sub-layer     :      11584
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44891E+01     640   0.24477E+00   0.94854E+01 0.42000E+01 
c  Velocity[X]                                      0.26368E+01 
c  Velocity[Y]                                      0.46190E+01 
c  Velocity[Z]                                      0.22297E+01 
c  Pressure     0.10921E+00     942   0.83535E-02   0.24046E-01 0.51197E-01 
c  k            0.51142E+00     153   0.70741E-04   0.89806E-03 0.14734E+01 
c  epsilon      0.33651E+04      88   0.54102E-03   0.79946E+06 0.14105E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k        
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6118      2.6965e+06          597.93          81.645


 TIME FOR THE TIME STEP              667:        0.17892E+03

===============================================================


 INSTANT    0.668000000E+02   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        -0.427334065E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888689E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
----------------------------------------------------------
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6118      2.6965e+06          597.93          81.645


 TIME FOR THE TIME STEP              667:        0.17948E+03

===============================================================


 INSTANT    0.668000000E+02   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        -0.427334065E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888689E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16224E+02 0.53559E+01
   Friction velocity        uet   :  0.24350E-01 0.29218E+02
   Friction velocity        uk    :  0.41475E-01 0.29218E+02
   Dimensionless distance   yplus :  0.24308E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13046
   Nb of faces within the viscous sub-layer     :      11584
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44891E+01     640   0.24477E+00   0.94854E+01 0.42000E+01 
c  Velocity[X]                                      0.26368E+01 
c  Velocity[Y]                                      0.46190E+01 
c  Velocity[Z]                                      0.22297E+01 
c  Pressure     0.10921E+00     942   0.83535E-02   0.24046E-01 0.51197E-01 
c  k            0.51142E+00     153   0.70741E-04   0.89806E-03 0.14734E+01 
c  epsilon      0.33651E+04      88   0.54102E-03   0.79946E+06 0.14105E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00082175                             9
a  epsilon                 -22.839                            12
a  Local Time Step      1.5484e-08                        281781


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3635          13.786          1.5462         0.37543
v  Velocity[Y]             -10.713          15.406           1.313         0.89353
v  Velocity[Z]             -18.133          11.094         -1.0218       -0.014296
v  ǁVelocityǁ             0.016404          20.555          6.0064            7.11
v  Pressure                 -26577      1.8942e+05      1.2421e+05           99586
v  k                    5.1155e-07          4.9723        0.066554         0.10209
v  epsilon               0.0065105      1.1637e+06          1574.9          54.307
v  TurbVisc             1.2689e-12         0.49487       0.0032832        0.047415
v  CourantNb              0.053168      6.4585e+05          382.85          78.303
v  FourierNb               0.22713      2.3653e+06          218.93          3.4073
v  total_pressure       4.7342e+05      6.8942e+05      6.2421e+05      5.9959e+05
v  Local Time Step            0.01        0.057132            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6319      2.7412e+06          601.79           81.71


 TIME FOR THE TIME STEP              668:        0.18360E+03

===============================================================


 INSTANT    0.669000000E+02   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         0.139692553E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888691E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
---------------------------------------------a  k                    -0.0020052                            32
a  epsilon                 -93.287                            41
a  Local Time Step      1.2473e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2977          13.641           1.564         0.37611
v  Velocity[Y]             -10.783          15.619          1.2833         0.89485
v  Velocity[Z]             -16.263          11.543        -0.99795       -0.013982
v  ǁVelocityǁ             0.020006           18.87           5.969          7.1155
v  Pressure                 -26540      1.8945e+05      1.2421e+05           99609
v  k                    2.2797e-07          5.0979        0.066166         0.10203
v  epsilon               0.0017512      1.1923e+06          1556.5          54.157
v  TurbVisc             1.2597e-12         0.49487       0.0032917        0.047413
v  CourantNb               0.19387      8.0174e+05          382.02           78.18
v  FourierNb               0.22704      2.3653e+06          218.95          3.4064
v  total_pressure       4.7346e+05      6.8945e+05      6.2421e+05      5.9961e+05
v  Local Time Step            0.01        0.062845            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6a  k                    -0.0020052                            32
a  epsilon                 -93.287                            41
a  Local Time Step      1.2473e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2977          13.641           1.564         0.37611
v  Velocity[Y]             -10.783          15.619          1.2833         0.89485
v  Velocity[Z]             -16.263          11.543        -0.99795       -0.013982
v  ǁVelocityǁ             0.020006           18.87           5.969          7.1155
v  Pressure                 -26540      1.8945e+05      1.2421e+05           99609
v  k                    2.2797e-07          5.0979        0.066166         0.10203
v  epsilon               0.0017512      1.1923e+06          1556.5          54.157
v  TurbVisc             1.2597e-12         0.49487       0.0032917        0.047413
v  CourantNb               0.19387      8.0174e+05          382.02           78.18
v  FourierNb               0.22704      2.3653e+06          218.95          3.4064
v  total_pressure       4.7346e+05      6.8945e+05      6.2421e+05      5.9961e+05
v  Local Time Step            0.01        0.062845            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6018      2.9273e+06          600.97          81.586


 TIME FOR THE TIME STEP              669:        0.17242E+03

===============================================================


 INSTANT    0.670000000E+02   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        -0.151859875E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888697E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
----------------------------------   Dimensionless distance   yplus :  0.27693E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13064
   Nb of faces within the viscous sub-layer     :      11609
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44874E+01     627   0.23955E+00   0.11112E+02 0.45408E+01 
c  Velocity[X]                                      0.27651E+01 
c  Velocity[Y]                                      0.65694E+01 
c  Velocity[Z]                                      0.17780E+01 
c  Pressure     0.10089E+00     921   0.77747E-02   0.22198E-01 0.40064E-01 
c  k            0.51127E+00     159   0.67800E-04   0.89296E-03 0.14696E+01 
c  epsilon      0.32789E+04      94   0.54039E-03   0.61437E+06 0.12641E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0011038                            54
a  epsilon                 -35.221                            69
a  Local Time Step      1.6023e-08                        281782


    Dimensionless distance   yplus :  0.27693E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13064
   Nb of faces within the viscous sub-layer     :      11609
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44874E+01     627   0.23955E+00   0.11112E+02 0.45408E+01 
c  Velocity[X]                                      0.27651E+01 
c  Velocity[Y]                                      0.65694E+01 
c  Velocity[Z]                                      0.17780E+01 
c  Pressure     0.10089E+00     921   0.77747E-02   0.22198E-01 0.40064E-01 
c  k            0.51127E+00     159   0.67800E-04   0.89296E-03 0.14696E+01 
c  epsilon      0.32789E+04      94   0.54039E-03   0.61437E+06 0.12641E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0011038                            54
a  epsilon                 -35.221                            69
a  Local Time Step      1.6023e-08                        281782


     Dimensionless distance   yplus :  0.27693E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13064
   Nb of faces within the viscous sub-layer     :      11609
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44874E+01     627   0.23955E+00   0.11112E+02 0.45408E+01 
c  Velocity[X]                                      0.27651E+01 
c  Velocity[Y]                                      0.65694E+01 
c  Velocity[Z]                                      0.17780E+01 
c  Pressure     0.10089E+00     921   0.77747E-02   0.22198E-01 0.40064E-01 
c  k            0.51127E+00     159   0.67800E-04   0.89296E-03 0.14696E+01 
c  epsilon      0.32789E+04      94   0.54039E-03   0.61437E+06 0.12641E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0011038                            54
a  epsilon                 -35.221                            69
a  Local Time Step      1.6023e-08                        281782


     Dimensionless distance   yplus :  0.27693E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13064
   Nb of faces within the viscous sub-layer     :      11609
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44874E+01     627   0.23955E+00   0.11112E+02 0.45408E+01 
c  Velocity[X]                                      0.27651E+01 
c  Velocity[Y]                                      0.65694E+01 
c  Velocity[Z]                                      0.17780E+01 
c  Pressure     0.10089E+00     921   0.77747E-02   0.22198E-01 0.40064E-01 
c  k            0.51127E+00     159   0.67800E-04   0.89296E-03 0.14696E+01 
c  epsilon      0.32789E+04      94   0.54039E-03   0.61437E+06 0.12641E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0011038                            54
a  epsilon                 -35.221                            69
a  Local Time Step      1.6023e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3922          13.633          1.5467         0.37557
v  Velocity[Y]             -10.738          15.848          1.3367         0.89352
v  Velocity[Z]             -18.351          9.3797         -1.0182       -0.013629
v  ǁVelocityǁ             0.014531           20.84          6.0293          7.1186
v  Pressure                 -26561      1.8945e+05       1.242e+05           99620
v  k                    4.4482e-08          4.9401        0.066045         0.10193
v  epsilon              8.6546e-05       1.124e+06          1533.2          54.107
v  TurbVisc             2.8475e-13         0.49487       0.0032734        0.047397
v  CourantNb               0.01301      6.2409e+05          377.83          78.245
v  FourierNb               0.22648      2.3653e+06          218.91          3.4068
v  total_pressure       4.7344e+05      6.8945e+05       6.242e+05      5.9962e+05
v  Local Time Step            0.01        0.076043        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
    INSTANT    0.673000000E+02   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        -0.188389151E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889068E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15893E+02 0.53654E+01
   Friction velocity        uet   :  0.38981E-01 0.54165E+02
   Friction velocity        uk    :  0.44445E-01 0.54165E+02
   Dimensionless distance   yplus :  0.44166E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13063
   Nb of faces within the viscous sub-layer     :      11563
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44868E+01     663   0.24564E+00   0.11477E+02 0.46154E+01 
c  Velocity[X]                                      0.31043E+01 
c  Velocity[Y]                                      0.62110E+01 
c  Velocity[Z]                                      0.21613E+01 
c  Pressure     0.10754E+00     742   0.81753E-02   0.23679E-01 0.22561E-01 
c  k            0.51131E+00     166   0.73646E-04   0.92220E-03 0.14929E+01 
c  epsilon      0.33748E+04      95   0.11045E-02   0.14766E+07 0.19021E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0010514                            15
a  epsilon                 -50.606                            35
a  Local Time Step       1.229e-08                        281780


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  INSTANT    0.673000000E+02   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        -0.188389151E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889068E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15893E+02 0.53654E+01
   Friction velocity        uet   :  0.38981E-01 0.54165E+02
   Friction velocity        uk    :  0.44445E-01 0.54165E+02
   Dimensionless distance   yplus :  0.44166E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13063
   Nb of faces INSTANT    0.673000000E+02   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        -0.188389151E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889068E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15893E+02 0.53654E+01
   Friction velocity        uet   :  0.38981E-01 0.54165E+02
   Friction velocity        uk    :  0.44445E-01 0.54165E+02
   Dimensionless distance   yplus :  0.44166E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13063
   Nb of faces within the viscous sub-layer     :      11563
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44868E+01     663   0.24564E+00   0.11477E+02 0.46154E+01 
c  Velocity[X]                                      0.31043E+01 
c  Velocity[Y]                                      0.62110E+01 
c  Velocity[Z]                                      0.21613E+01 
c  Pressure     0.10754E+00     742   0.81753E-02   0.23679E-01 0.22561E-01 
c  k            0.51131E+00     166   0.73646E-04   0.92220E-03 0.14929E+01 
c  epsilon      0.33748E+04      95   0.11045E-02   0.14766E+07 0.19021E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0010514                            15
a  epsilon                 -50.606                            35
a-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3147          13.609          1.5662         0.37604
v  Velocity[Y]              -10.77          15.533          1.2918         0.89467
v  Velocity[Z]             -15.371          9.8305        -0.99144       -0.013798
v  ǁVelocityǁ            0.0065135          18.436          5.9993          7.1133
v  Pressure                 -26607      1.8948e+05      1.2417e+05           99587
v  k                    1.6091e-07            4.84        0.065453         0.10197
v  epsilon              0.00066451      1.1536e+06          1506.7          53.971
v  TurbVisc             9.0384e-13         0.49487       0.0032927        0.047397
v  CourantNb               0.28105      6.3223e+05          376.36          78.232
v  FourierNb               0.22622      2.3653e+06          218.94          3.4084
v  total_pressure       4.7339e+05      6.8948e+05      6.2417e+05      5.9959e+05
v  Local Time Step            0.01         0.10121        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6077      2.7578e+06           595.3          81.641


 TIME FOR THE TIME STEP              674:        0.17997E+03

===============================================================


 INSTANT    0.675000000E+02   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         0.991029919E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889064E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16215E+02 0.52669E+01
   Friction velocity        uet   :  0.28050E-01 0.40007E+02
   Friction velocity        uk    :  0.45519E-01 0.40007E+02
   Dimensionless distance   yplus :  0.48992E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13038
   Nb of faces within the viscous sub-layer     :      11564
   Total number of wall faces                   :      41000
---------------------------------------------------  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3147          13.609          1.5662         0.37604
v  Velocity[Y]              -10.77          15.533          1.2918         0.89467
v  Velocity[Z]             -15.371          9.8305        -0.99144       -0.013798
v  ǁVelocityǁ            0.0065135          18.436          5.9993          7.1133
v  Pressure                 -26607      1.8948e+05      1.2417e+05           99587
v  k                    1.6091e-07            4.84        0.065453         0.10197
v  epsilon              0.00066451      1.1536e+06          1506.7          53.971
v  TurbVisc             9.0384e-13         0.49487       0.0032927        0.047397
v  CourantNb               0.28105      6.3223e+05          376.36          78.232
v  FourierNb               0.22622      2.3653e+06          218.94          3.4084
v  total_pressure       4.7339e+05      6.8948e+05      6.2417e+05      5.9959e+05
v  Local Time Step            0.01         0.10121        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6077      2.7578e+06           595.3          81.641


 TIME FOR THE TIME STEP              674:        0.18129E+03

===============================================================


 INSTANT    0.675000000E+02   TIME STEP NUMBER             675
 ============================================================= 




   ** BOUNDARY MASS FLOW INF-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3147          13.609          1.5662         0.37604
v  Velocity[Y]              -10.77          15.533          1.2918         0.89467
v  Velocity[Z]             -15.371          9.8305        -0.99144       -0.013798
v  ǁVelocityǁ            0.0065135          18.436          5.9993          7.1133
v  Pressure                 -26607      1.8948e+05      1.2417e+05           99587
v  k                    1.6091e-07            4.84        0.065453         0.10197
v  epsilon              0.00066451      1.1536e+06          1506.7          53.971
v  TurbVisc             9.0384e-13         0.49487       0.0032927        0.047397
v  CourantNb               0.28105      6.3223e+05          376.36          78.232
v  FourierNb               0.22622      2.3653e+06          218.94          3.4084
v  total_pressure       4.7339e+05      6.8948e+05      6.2417e+05      5.9959e+05
v  Local Time Step            0.01         0.10121        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6077      2.7578e+06           595.3          81.641


 TIME FOR THE TIME STEP              674:        0.18856E+03

===============================================================


 INSTANT    0.675000000E+02   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         0.991029919E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889064E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16215E+02 0.52669E+01
   Friction velocity        uet   :  0.28050E-01 0.40007E+02
   Friction velocity        uk    :  0.45519E-01 0.40007E+02
   Dimensionless distance   yplus :  0.48992E-02 0.23857E+02
   ----------------------------------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44926E+01     618   0.24017E+00   0.10683E+02 0.44534E+01 
c  Velocity[X]                                      0.29233E+01 
c  Velocity[Y]                                      0.52122E+01 
c  Velocity[Z]                                      0.25474E+01 
c  Pressure     0.10063E+00     945   0.76206E-02   0.22119E-01 0.58045E-01 
c  k            0.51131E+00     169   0.77931E-04   0.10283E-02 0.15768E+01 
c  epsilon      0.33114E+04     102   0.78672E-03   0.92065E+06 0.15322E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00052298                            30
a  epsilon                 -80.148                            57
a  Local Time Step      1.4361e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4601          13.638          1.5515         0.37539
v  Velocity[Y]             -10.815          15.335          1.3233         0.89344
v  Velocity[Z]             -15.544          10.635         -1.0135       -0.014107
v  ǁVelocityǁ            0.0093583          18.211          6.0381          7.1159
v  Pressure                 -26589      1.8947e+05      1.2418e+05           99568
v  k                    3.8317e-09          4.9417        0.066727         0.10201
v  epsilon               0.0055152      1.1441e+06          1556.7          54.309
v  TurbVisc             1.2491e-12         0.49487       0.0032879          0.0474
v  CourantNb               0.19638      6.9632e+05          382.32          78.318
v  FourierNb               0.22626      2.3653e+06          218.93          3.4075
v  total_pressure       4.7341e+05      6.8947e+05      6.2418e+05      5.9957e+05
v  Local Time Step            0.01        0.075326        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6001      2.8219e+06          601.25          81.726


 TIME FOR THE TIME STEP              676:        0.18040E+03

===============================================================


 INSTANT    0.677000000E+02   TIME STEP NUMBER             677
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces         ------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44926E+01     618   0.24017E+00   0.10683E+02 0.44534E+01 
c  Velocity[X]                                      0.29233E+01 
c  Velocity[Y]                                      0.52122E+01 
c  Velocity[Z]                                      0.25474E+01 
c  Pressure     0.10063E+00     945   0.76206E-02   0.22119E-01 0.58045E-01 
c  k            0.51131E+00     169   0.77931E-04   0.10283E-02 0.15768E+01 
c  epsilon      0.33114E+04     102   0.78672E-03   0.92065E+06 0.15322E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00052298                            30
a  epsilon                 -80.148                            57
a  Local Time Step      1.4361e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4601          13.638          1.5515         0.------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44926E+01     618   0.24017E+00   0.10683E+02 0.44534E+01 
c  Velocity[X]                                      0.29233E+01 
c  Velocity[Y]                                      0.52122E+01 
c  Velocity[Z]                                      0.25474E+01 
c  Pressure     0.10063E+00     945   0.76206E-02   0.22119E-01 0.58045E-01 
c  k            0.51131E+00     169   0.77931E-04   0.10283E-02 0.15768E+01 
c  epsilon      0.33114E+04     102   0.78672E-03   0.92065E+06 0.15322E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00052298                            30
a  epsilon                 -80.148                            57
a  Local Time Step      1.4361e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4601          13.638          1.5515         0.37539
v  Velocity[Y]             -10.815          15.335          1.3233         0.89344
v  Velocity[Z]             -15.544          10.635         -1.0135       -0.014107
v  ǁVelocityǁ            0.0093583          18.211          6.0381          7.1159
v  Pressure                 -26589      1.8947e+05      1.2418e+05           99568
v  k                    3.8317e-09          4.9417        0.066727         0.10201
v  epsilon               0.0055152      1.1441e+06          1556.7          54.309
v  TurbVisc             1.2491e-12         0.49487       0.0032879          0.0474
v  CourantNb               0.19638      6.9632e+05          382.32          78.318
v  FourierNb               0.22626      2.3653e+06          218.93          3.4075
v  total_pressure       4.7341e+05      6.8947e+05      6.2418e+05      5.9957e+05
v  Local Time Step            0.01        0.075326        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6001      2.8219e+06          601.25          81.726


 TIME FOR THE TIME STEP              676:        0.18344E+03

===============================================================


 INSTANT    0.677000000E+02   TIME STEP NUMBER             6Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.920021679E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888707E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15837E+02 0.53849E+01
   Friction velocity        uet   :  0.35386E-01 0.28985E+02
   Friction velocity        uk    :  0.36929E-01 0.28985E+02
   Dimensionless distance   yplus :  0.36986E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13058
   Nb of faces within the viscous sub-layer     :      11591
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44950E+01     652   0.24180E+00   0.10116E+02 0.43367E+01 
c  Velocity[X]                                      0.29875E+01 
c  Velocity[Y]                                      0.49441E+01 
c  Velocity[Z]                                      0.21844E+01 
c  Pressure     0.98915E-01     897   0.75146E-02   0.21742E-01 0.31821E-01 
c  k            0.51127E+00     166   0.80553E-04   0.10525E-02 0.15956E+01 
c  epsilon      0.33483E+04     101   0.58274E-03   0.10391E+07 0.16287E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0025141                            16
a  epsilon                 -64.887                            26
a  Local Time Step      1.6127e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4166          13.629          1.5702         0.37681
v  Velocity[Y]              -10.79          15.696           1.275         0.89518
v  Velocity[Z]             -17.899          10.398        -0.99572      Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.920021679E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888707E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15837E+02 0.53849E+01
   Friction velocity        uet   :  0.35386E-01 0.28985E+02
   Friction velocity        uk    :  0.36929E-01 0.28985E+02
   Dimensionless distance   yplus :  0.36986E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13058
   Nb of faces within the viscous sub-layer     :      11591
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
--------------------------------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.920021679E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888707E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15837E+02 0.53849E+01
   Friction velocity        uet   :  0.35386E-01 0.28985E+02
   Friction velocity        uk    :  0.36929E-01 0.28985E+02
   Dimensionless distance   yplus :  0.36986E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13058
   Nb of faces within the viscous sub-layer     :      11591
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44950E+01     652   0.24180E+00   0.10116E+02 0.43367E+01 
c  Velocity[X]                                      0.29875E+01 
c  Velocity[Y]                                      0.49441E+01 
c  Velocity[Z]                                      0.21844E+01 
c  Pressure     0.98915E-01     897   0.75146E-02   0.21742E-01 0.31821E-01 
c  k            0.51127E+00     166   0.80553E-04   0.10525E-02 0.15956E+01 
c  epsilon      0.33483E+04     101   0.58274E-03   0.10391E+07 0.16287E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0025141                            16
a  epsilon                 -64.887                            26
a  Local Time Step      1.6127e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  ---v  Velocity[Z]             -14.728          10.836         -1.0241       -0.013492
v  ǁVelocityǁ             0.016507          18.349          6.0207          7.1191
v  Pressure                 -26501      1.8953e+05       1.242e+05           99630
v  k                    3.2401e-07          4.8645        0.065679         0.10196
v  epsilon               0.0061028      1.0977e+06            1484          53.971
v  TurbVisc             1.2811e-12         0.49487       0.0032902        0.047395
v  CourantNb              0.054534      6.8542e+05          377.54          78.236
v  FourierNb               0.22608      2.3653e+06          218.92          3.4083
v  total_pressure        4.735e+05      6.8953e+05       6.242e+05      5.9963e+05
v  Local Time Step            0.01         0.10026        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6256      2.7472e+06          596.46          81.644


 TIME FOR THE TIME STEP              679:        0.17666E+03

===============================================================


 INSTANT    0.680000000E+02   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         0.103902010E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889092E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16040E+02 0.52811E+01
   Friction velocity        uet   :  0.35082E-01 0.40696E+02
   Friction velocity        uk    :  0.45280E-01 0.40696E+02
   Dimensionless distance   yplus :  0.45306E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13099
   Nb of faces within the viscous sub-layer     :      11595
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-------------v  Velocity[Z]             -14.728          10.836         -1.0241       -0.013492
v  ǁVelocityǁ             0.016507          18.349          6.0207          7.1191
v  Pressure                 -26501      1.8953e+05       1.242e+05           99630
v  k                    3.2401e-07          4.8645        0.065679         0.10196
v  epsilon               0.0061028      1.0977e+06            1484          53.971
v  TurbVisc             1.2811e-12         0.49487       0.0032902        0.047395
v  CourantNb              0.054534      6.8542e+05          377.54          78.236
v  FourierNb               0.22608      2.3653e+06          218.92          3.4083
v  total_pressure        4.735e+05      6.8953e+05       6.242e+05      5.9963e+05
v  Local Time Step            0.01         0.10026        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6256      2.7472e+06          596.46          81.644


 TIME FOR THE TIME STEP              679:        0.18041E+03

===============================================================


 INSTANT    0.680000000E+02   TIME STEP NUMBER             680
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet         v  Velocity[Z]             -14.728          10.836         -1.0241       -0.013492
v  ǁVelocityǁ             0.016507          18.349          6.0207          7.1191
v  Pressure                 -26501      1.8953e+05       1.242e+05           99630
v  k                    3.2401e-07          4.8645        0.065679         0.10196
v  epsilon               0.0061028      1.0977e+06            1484          53.971
v  TurbVisc             1.2811e-12         0.49487       0.0032902        0.047395
v  CourantNb              0.054534      6.8542e+05          377.54          78.236
v  FourierNb               0.22608      2.3653e+06          218.92          3.4083
v  total_pressure        4.735e+05      6.8953e+05       6.242e+05      5.9963e+05
v  Local Time Step            0.01         0.10026        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6256      2.7472e+06          596.46          81.644


 TIME FOR THE TIME STEP              679:        0.17410E+03

===============================================================


 INSTANT    0.680000000E+02   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         0.103902010E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889092E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16040E+02 0.52811E+01
   Friction velocity        uet   :  0.35082E-01 0.40696E+02
   Friction velocity        uk    :  0.45280E-01 0.40696E+02
   Dimensionless distance   yplus :  0.45306E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13099
   Nb of faces within the viscous sub-layer     :      11595
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44961E+01     639   0.23998E+00   0.11903E+02 0.46991E+01 
c  Velocity[X]                                      0.35083E+01 
c  Velocity[Y]                                      0.62809E+01 
c  Velocity[Z]                                      0.21139E+01 
c  Pressure     0.10336E+00     796   0.78535E-02   0.22709E-01 0.36467E-01 
c  k            0.51128E+00     168   0.88287E-04   0.10812E-02 0.16170E+01 
c  epsilon      0.32659E+04      98   0.98868E-03   0.15270E+07 0.19739E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0018418                            24
a  epsilon                 -19.777                            41
a  Local Time Step      1.3128e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.543          13.701          1.5524         0.37513
v  Velocity[Y]              -10.73          15.362          1.3357         0.89348
v  Velocity[Z]             -17.848          10.164         -1.0267       -0.014158
v  ǁVelocityǁ             0.019352          20.409          6.0483          7.1195
v  Pressure                 -26552      1.8955e+05      1.2422e+05           99648
v  k                    9.9451e-08          4.8494        0.066983         0.10199
v  epsilon               0.0067233       1.125e+06          1570.1          54.351
v  TurbVisc             1.2185e-12         0.49487       0.0032916        0.047393
v  CourantNb              0.039498      7.6175e+05          382.08          78.335
v  FourierNb               0.22597      2.3653e+06          218.93          3.4074
v  total_pressure       4.7345e+05      6.8955e+05      6.2422e+05      5.9965e+05
v  Local Time Step            0.01         0.11029        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6687      2.8874e+06          601.02          81.742


 TIME FOR THE TIME STEP              680:        0.18050E+03

===============================================================


 INSTANT    0.681000000E+02   TIME STEP NUMBER             681
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
-----------------------------------------------------------------------------
c  Velocity     0.44950E+01     630   0.24583E+00   0.11387E+02 0.45978E+01 
c  Velocity[X]                                      0.27628E+01 
c  Velocity[Y]                                      0.62345E+01 
c  Velocity[Z]                                      0.23893E+01 
c  Pressure     0.10178E+00     742   0.79165E-02   0.22360E-01 0.30218E-01 
c  k            0.51137E+00     162   0.72261E-04   0.93601E-03 0.15043E+01 
c  epsilon      0.33898E+04     100   0.72296E-03   0.87527E+06 0.14627E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00016978                            11
a  epsilon                 -19.982                            21
a  Local Time Step      1.4215e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2736          13.688          1.5485         0.37512
v  Velocity[Y]             -10.709          15.804          1.3034         0.89471
v  Velocity[Z]             -15.086          11.565         -1.0033       -0.014822
v  ǁVelocityǁ             0.016922          18.508          6.0233          7.1151
v  Pressure                 ------------------------------------------------------------------------------
c  Velocity     0.44950E+01     630   0.24583E+00   0.11387E+02 0.45978E+01 
c  Velocity[X]                                      0.27628E+01 
c  Velocity[Y]                                      0.62345E+01 
c  Velocity[Z]                                      0.23893E+01 
c  Pressure     0.10178E+00     742   0.79165E-02   0.22360E-01 0.30218E-01 
c  k            0.51137E+00     162   0.72261E-04   0.93601E-03 0.15043E+01 
c  epsilon      0.33898E+04     100   0.72296E-03   0.87527E+06 0.14627E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00016978                            11
a  epsilon                 -19.982                            21
a  Local Time Step      1.4215e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2736          13.688          1.5485         0.37512
v  Velocity[Y]             -10.709          15.804          1.3034         0.89471
v  Velocity[Z]             -15.086          11.565         -1.0033       -0.014822
v  ǁVelocityǁ             0.016922          18.508          6.0233          7.1151
v  Pressure                 -26609      1.8961e+05      1.2423e+05           99652
v  k                     4.223e-07          5.1453        0.066774         0.10203
v  epsilon               0.0015722      1.1516e+06          1586.7          54.295
v  TurbVisc             1.6947e-12         0.49487       0.0032878        0.047394
v  CourantNb               0.31603       7.035e+05          385.58          78.407
v  FourierNb               0.22603      2.3653e+06          218.94          3.4072
v  total_pressure       4.7339e+05      6.8961e+05      6.2423e+05      5.9965e+05
v  Local Time Step            0.01        0.064763            0.01        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.591      2.8291e+06          604.51          81.814


 TIME FOR THE TIME STEP              681:        0.17736E+03

===============================================================


 INSTANT    0.682000000E+02   TIME STEP NUMBER             682
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
----------------------------------------------Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889069E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16030E+02 0.52669E+01
   Friction velocity        uet   :  0.37311E-01 0.24823E+02
   Friction velocity        uk    :  0.45433E-01 0.24823E+02
   Dimensionless distance   yplus :  0.29160E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13055
   Nb of faces within the viscous sub-layer     :      11620
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44920E+01     627   0.24412E+00   0.97193E+01 0.42485E+01 
c  Velocity[X]                                      0.29964E+01 
c  Velocity[Y]                                      0.44226E+01 
c  Velocity[Z]                                      0.23003E+01 
c  Pressure     0.10059E+00     869   0.80850E-02   0.22115E-01 0.33127E-01 
c  k            0.51134E+00     167   0.89726E-04   0.12598E-02 0.17452E+01 
c  epsilon      0.32238E+04      96   0.11722E-02   0.21401E+07 0.24332E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0079724                            44
a  epsilon                 -891.42                            87
a  Local Time Step       1.427e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1583           13.63          1.5611          0.3759
v  Velocity[Y]             -10.798           15.62          1.3017         0.89428
v  Velocity[Z]             -17.219          12.421         -1.0215       -0.013556
v  ǁVelocityǁ              0.01819          19.807          6.0132          7.1164
v  Pressure                 -26582       1.895e+05      1.2414e+05           99590
v  k                    4.3869e-07          4.8334        0.065366         0.10212
v  epsilon               0.0024427      1.0914e+06    Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889069E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16030E+02 0.52669E+01
   Friction velocity        uet   :  0.37311E-01 0.24823E+02
   Friction velocity        uk    :  0.45433E-01 0.24823E+02
   Dimensionless distance   yplus :  0.29160E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13055
   Nb of faces within the viscous sub-layer     :      11620
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44920E+01     627   0.24412E+00   0.97193E+01 0.42485E+01 
c  Velocity[X]                       Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889069E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16030E+02 0.52669E+01
   Friction velocity        uet   :  0.37311E-01 0.24823E+02
   Friction velocity        uk    :  0.45433E-01 0.24823E+02
   Dimensionless distance   yplus :  0.29160E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13055
   Nb of faces within the viscous sub-layer     :      11620
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44920E+01     627   0.24412E+00   0.97193E+01 0.42485E+01 
c  Velocity[X]                                      0.29964E+01 
c  Velocity[Y]                                      0.44226E+01 
c  Velocity[Z]                                      0.23003E+01 
c  Pressure     0.10059E+00     869   0.80850E-02   0.22115E-01 0.33127E-01 
c  k            0.51134E+00     167   0.89726E-04   0.12598E-02 0.17452E+01 
c  epsilon      0.32238E+04      96   0.11722E-02   0.21401E+07 0.24332E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0079724                            44
a  epsilon                 -891.42                            87
a  Local Time Step       1.427e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1583           13.63          1.5611          0.3759
v  Velocity[Y]             -10.798           15.62          1.3017         0.89428
v  Velocity[Z]             -17.219          12.421         -1.0215       -0.013556
v  ǁVelocityǁ              0.01819     v  epsilon              0.00077549      1.1191e+06          1544.3          54.283
v  TurbVisc             1.6022e-12         0.49487       0.0032904        0.047415
v  CourantNb               0.14045      8.1002e+05          380.24          78.323
v  FourierNb               0.22668      2.3653e+06          218.92          3.4078
v  total_pressure       4.7337e+05      6.8943e+05      6.2407e+05      5.9953e+05
v  Local Time Step            0.01        0.066214        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6241      2.9356e+06          599.16          81.731


 TIME FOR THE TIME STEP              684:        0.17455E+03

===============================================================


 INSTANT    0.685000000E+02   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         0.639833249E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889061E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15841E+02 0.52869E+01
   Friction velocity        uet   :  0.39522E-01 0.39357E+02
   Friction velocity        uk    :  0.44254E-01 0.39357E+02
   Dimensionless distance   yplus :  0.41195E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13124
   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     0.44928E+01     606   0.24522E+00   0.10494E+02 0.44141E+01 
c  Velocity[X]                                      0.28104E+01 
c  Velocity[Y]                                      0.51654E+01 
c  Velocity[Z]                                      0.25184E+0v  epsilon              0.00077549      1.1191e+06          1544.3          54.283
v  TurbVisc             1.6022e-12         0.49487       0.0032904        0.047415
v  CourantNb               0.14045      8.1002e+05          380.24          78.323
v  FourierNb               0.22668      2.3653e+06          218.92          3.4078
v  total_pressure       4.7337e+05      6.8943e+05      6.2407e+05      5.9953e+05
v  Local Time Step            0.01        0.066214        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6241      2.9356e+06          599.16          81.731


 TIME FOR THE TIME STEP              684:        0.18190E+03

===============================================================


 INSTANT    0.685000000E+02   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         0.639833249E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889061E+01
Free inlet               13 v  epsilon              0.00077549      1.1191e+06          1544.3          54.283
v  TurbVisc             1.6022e-12         0.49487       0.0032904        0.047415
v  CourantNb               0.14045      8.1002e+05          380.24          78.323
v  FourierNb               0.22668      2.3653e+06          218.92          3.4078
v  total_pressure       4.7337e+05      6.8943e+05      6.2407e+05      5.9953e+05
v  Local Time Step            0.01        0.066214        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6241      2.9356e+06          599.16          81.731


 TIME FOR THE TIME STEP              684:        0.18347E+03

===============================================================


 INSTANT    0.685000000E+02   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         0.639833249E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889061E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15841E+02 0.52869E+01
   Friction velocity        uet   :  0.39522E-01 0.39357E+02
   Friction velocity        uk    :  0.44254E-01 0.39357E+02
   Dimensionless distance   yplus :  0.41195E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13124
   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     0.44928E+01     606   0.24522E+00   0.10494E+02 0.44141E+01 
c  Velocity[X]                                      0.28104E+01 
c  Velocity[Y]                                      0.51654E+01 
c  Velocity[Z]                                      0.25184E+01 
c  Pressure     0.10079E+00     782   0.74371E-02   0.22141E-01 0.36959E-01 
c  k            0.51134E+00     158   0.84891E-04   0.11528E-02 0.16694E+01 
c  epsilon      0.33384E+04     107   0.79619E-03   0.15130E+07 0.19372E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -5.104e-05                             9
a  epsilon                 -12.548                            12
a  Local Time Step      1.5294e-08                        281777


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2589          13.739          1.5477         0.37513
v  Velocity[Y]              -10.75          15.544           1.318         0.89406
v  Velocity[Z]             -17.108          9.5525          -1.003       -0.014864
v  ǁVelocityǁ             0.026515          19.692          6.0521          7.1157
v  Pressure                 -26685      1.8944e+05      1.2406e+05           99506
v  k                    4.5073e-07          5.0284        0.066675         0.10209
v  epsilon                0.001834      1.1117e+06          1582.6          54.414
v  TurbVisc             1.5514e-12         0.49487       0.0032934        0.047416
v  CourantNb              0.068749      6.5387e+05          383.25           78.37
v  FourierNb               0.22673      2.3653e+06          218.93          3.4089
v  total_pressure       4.7332e+05      6.8944e+05      6.2406e+05      5.9951e+05
v  Local Time Step            0.01        0.072835        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6324      2.7218e+06          602.18          81.779


 TIME FOR THE TIME STEP              685:        0.16940E+03

===============================================================


 INSTANT    0.686000000E+02   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         0.130088488E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3  c  Velocity[Z]                                      0.19212E+01 
c  Pressure     0.10126E+00     871   0.76868E-02   0.22271E-01 0.22133E-01 
c  k            0.51135E+00     166   0.76569E-04   0.10516E-02 0.15947E+01 
c  epsilon      0.34172E+04      95   0.10100E-02   0.13958E+07 0.18275E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0060858                             9
a  epsilon                 -149.84                            20
a  Local Time Step      1.4066e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5509          13.723          1.5712         0.37507
v  Velocity[Y]             -10.903          15.491          1.2932         0.89519
v  Velocity[Z]             -14.836          11.312         -1.0074       -0.014237
v  ǁVelocityǁ            0.0074578          18.301          5.9889           7.117
v  Pressure                 -26710      1.8942e+05      1.2402e+05           99492
v  k                    4.1197e-07          5.6724        0.066797         0.10206
v  epsilon               0.0022269      1.3666e+06          1593.7          54.332
v  TurbVisc             1.4849e-12         0.49487       0.003291c  Velocity[Z]                                      0.19212E+01 
c  Pressure     0.10126E+00     871   0.76868E-02   0.22271E-01 0.22133E-01 
c  k            0.51135E+00     166   0.76569E-04   0.10516E-02 0.15947E+01 
c  epsilon      0.34172E+04      95   0.10100E-02   0.13958E+07 0.18275E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0060858                             9
a  epsilon                 -149.84                            20
a  Local Time Step      1.4066e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5509          13.723          1.5712         0.37507
v  Velocity[Y]             -10.903          15.491          1.2932         0.89519
v  Velocity[Z]             -14.836          11.312         -1.0074       -0.014237
v  ǁVelocityǁ            0.0074578          18.301          5.9889           7.117
v  Pressure                 -26710      1.8942e+05      1.2402e+05           99492
v  k                    4.1197e-07          5.6724        0.066797         0.10206
v  epsilon               0.0022269      1.3666e+06          1593.7          54.332
v  TurbVisc             1.4849e-12         0.49487       0.0032916        0.047411
v  CourantNb               0.19141      7.1092e+05          385.31          78.345
v  FourierNb               0.22669      2.3653e+06          218.95          3.4082
v  total_pressure       4.7329e+05      6.8942e+05      6.2402e+05      5.9949e+05
v  Local Time Step            0.01        0.080119        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6511      2.6964e+06          604.27          81.753


 TIME FOR THE TIME STEP              686:        0.18378E+03

===============================================================


 INSTANT    0.687000000E+02   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        -0.757569817E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0       Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15814E+02 0.52920E+01
   Friction velocity        uet   :  0.24724E-01 0.47443E+02
   Friction velocity        uk    :  0.24780E-01 0.47443E+02
   Dimensionless distance   yplus :  0.35069E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13076
   Nb of faces within the viscous sub-layer     :      11655
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44877E+01     657   0.24300E+00   0.11243E+02 0.45674E+01 
c  Velocity[X]                                      0.26739E+01 
c  Velocity[Y]                                      0.63845E+01 
c  Velocity[Z]                                      0.21849E+01 
c  Pressure     0.10395E+00     898   0.78086E-02   0.22875E-01 0.37651E-01 
c  k            0.51131E+00     155   0.56610E-04   0.70109E-03 0.13021E+01 
c  epsilon      0.32597E+04     102   0.30672E-03   0.28733E+06 0.87535E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00069004                            10
a  epsilon                 -9.0537                            14
a  Local Time Step      1.3024e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5564          13.504          1.5461         0.37555
v  Velocity[Y]             -10.667          15.264          1.3132         0.89448
v  Velocity[Z]             -15.359          10.466          -1.012       -0.013925
v  ǁVelocityǁ             0.017146           18.06          6.0223           7.118
v  Pressure                 -26770      1.8935e+05      1.2398e+05           99468
v  k                    1.9168e-09          4.8533        0.065615         0.10202
v  epsilon               0.0011925      1.1334e+06          1497.7           53.99
v  TurbVisc             1.4831e-12         0.49487       0.0032848        0.047403
v  CourantNb               0.15629      7.6784e+05          378.43          78.325
v  FourierNb               0.22631      2.3653e+06          2Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15814E+02 0.52920E+01
   Friction velocity        uet   :  0.24724E-01 0.47443E+02
   Friction velocity        uk    :  0.24780E-01 0.47443E+02
   Dimensionless distance   yplus :  0.35069E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13076
   Nb of faces within the viscous sub-layer     :      11655
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44877E+01     657   0.24300E+00   0.11243E+02 0.45674E+01 
c  Velocity[X]                                      0.26739E+01 
c  Velocity[Y]                                      0.63845E+01 
c  Velocity[Z]                                      0.21849E+01 
c  Pressure     0.10395E+00     898   0.78086E-02   0.22875E-01 0.37651E-01 
c  k            0.511Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15814E+02 0.52920E+01
   Friction velocity        uet   :  0.24724E-01 0.47443E+02
   Friction velocity        uk    :  0.24780E-01 0.47443E+02
   Dimensionless distance   yplus :  0.35069E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13076
   Nb of faces within the viscous sub-layer     :      11655
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44877E+01     657   0.24300E+00   0.11243E+02 0.45674E+01 
c  Velocity[X]                                      0.26739E+01 
c  Velocity[Y]                                      0.63845E+01 
c  Velocity[Z]                                      0.21849E+01 
c  Pressure     0.10395E+00     898   0.78086E-02   0.22875E-01 0.37651E-01 
c  k            0.51131E+00     155   0.56610E-04   0.70109E-03 0.13021E+01 
c  epsilon      0.32597E+04     102   0.30672E-03   0.28733E+06 0.87535E+01 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00069004                            10
a  epsilon                 -9.0537                            14
a  Local Time Step      1.3024e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5564          13.504          1.5461         0.37555
v  Velocity[Y]             -10.667          15.264          1.3132         0.89448
v  Velocity[Z]             -15.359          10.466          -1.012       -0.013925
v  ǁVelocityǁ             0.017146           18.06          6.0223           7.118
v  Pressure                 -26770      1.8935e+05      1.2398e+05           99468
v  k                    1.9168e-09          4.8533        0.065615         0.10202
v  epsilon               0.0011925     v  FourierNb                0.2262      2.3653e+06          218.93          3.4075
v  total_pressure       4.7323e+05      6.8938e+05        6.24e+05      5.9947e+05
v  Local Time Step            0.01        0.072924        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5947      2.6653e+06          600.76          81.693


 TIME FOR THE TIME STEP              689:        0.17693E+03

===============================================================


 INSTANT    0.690000000E+02   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         0.105316049E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888694E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16376E+02 0.54249E+01
   Friction velocity        uet   :  0.34846E-01 0.38948E+02
   Friction velocity        uk    :  0.40367E-01 0.38948E+02
   Dimensionless distance   yplus :  0.38226E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13060
   Nb of faces within the viscous sub-layer     :      11563
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44916E+01     678   0.24802E+00   0.12075E+02 0.47339E+01 
c  Velocity[X]                                      0.30108E+01 
c  Velocity[Y]                                      0.68516E+01 
c  Velocity[Z]                                      0.22129E+01 
c  Pressure     0.10300E+00     873   0.78153E-02   0.22666E-01 0.38906E-01 
c  k            0.51144E+00     163   0.78673E-04   0.10291E-02 0.15773E+01 
c  epsilon      0.34353E+04      94   0.11869E-02   0.18474E+07 0.20809E+02 
---------------v  FourierNb                0.2262      2.3653e+06          218.93          3.4075
v  total_pressure       4.7323e+05      6.8938e+05        6.24e+05      5.9947e+05
v  Local Time Step            0.01        0.072924        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5947      2.6653e+06          600.76          81.693


 TIME FOR THE TIME STEP              689:        0.17547E+03

===============================================================


 INSTANT    0.690000000E+02   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         0.105316049E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888694E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------v  FourierNb                0.2262      2.3653e+06          218.93          3.4075
v  total_pressure       4.7323e+05      6.8938e+05        6.24e+05      5.9947e+05
v  Local Time Step            0.01        0.072924        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5947      2.6653e+06          600.76          81.693


 TIME FOR THE TIME STEP              689:        0.17096E+03

===============================================================


 INSTANT    0.690000000E+02   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         0.105316049E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888694E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16376E+02 0.54249E+01
   Friction velocity        uet   :  0.34846E-01 0.38948E+02
   Friction velocity        uk    :  0.40367E-01 0.38948E+02
   Dimensionless distance   yplus :  0.38226E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13060
   Nb of faces within the viscous sub-layer     :      11563
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44916E+01     678   0.24802E+00   0.12075E+02 0.47339E+01 
c  Velocity[X]                                      0.30108E+01 
c  Velocity[Y]                                      0.68516E+01 
c  Velocity[Z]                                      0.22129E+01 
c  Pressure     0.10300E+00     873   0.78153E-02   0.22666E-01 0.38906E-01 
c  k            0.51144E+00     163   0.78673E-04   0.10291E-02 0.15773E+01 
c  epsilon      0.34353E+04      94   0.11869E-02   0.18474E+07 0.20809E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0046307                            22
a  epsilon                 -114.57                            40
a  Local Time Step      1.3528e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5333          13.646          1.5763         0.37414
v  Velocity[Y]             -10.794          15.603          1.2925         0.89363
v  Velocity[Z]             -14.547          9.8415         -1.0085       -0.014448
v  ǁVelocityǁ             0.009494           18.34          5.9811          7.1162
v  Pressure                 -26753      1.8944e+05      1.2403e+05           99510
v  k                    4.6702e-07          5.6616        0.067062         0.10213
v  epsilon               0.0072522      1.3644e+06          1611.9          54.465
v  TurbVisc             1.4343e-12         0.49487       0.0032984        0.047406
v  CourantNb               0.22368      7.3923e+05          386.84          78.381
v  FourierNb               0.22644      2.3653e+06          218.95           3.408
v  total_pressure       4.7325e+05      6.8944e+05      6.2403e+05      5.9951e+05
v  Local Time Step            0.01        0.080217        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5907      2.7211e+06          605.79          81.789


 TIME FOR THE TIME STEP              690:        0.18120E+03

===============================================================


 INSTANT    0.691000000E+02   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         0.179884880E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888692E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
----------------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0027299                            37
a  epsilon                 -133.48                            86
a  Local Time Step       1.225e-08                        281787


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3933          13.568          1.5806          0.3756
v  Velocity[Y]             -10.691          16.168          1.2825         0.89431
v  Velocity[Z]             -17.425          10.658        -0.99193       -0.014502
v  ǁVelocityǁ             0.010281          19.973          5.9922          7.1158
v  Pressure                 -26714       1.894e+05      1.2401e+05           99491
v  k                    3.2146e-07          4.9358         0.06529         0.10212
v  epsilon               0.0041652      1.1069e+06            1481          54.048
v  TurbVisc             1.6006e-12         0.49487       0.0033124        0.047417
v  CourantNb               0.57989      8.1631e+05          379.11          78.211
v  FourierNb               0.22664      2.3653e+06          218.96          3.4092
v  total_pressure       4.7329e+05       6.894e+05      6.2401e+05      5.9949e+05
v  Local Time Step           -----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0027299                            37
a  epsilon                 -133.48                            86
a  Local Time Step       1.225e-08                        281787


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3933          13.568          1.5806          0.3756
v  Velocity[Y]             -10.691          16.168          1.2825         0.89431
v  Velocity[Z]             -17.425          10.658        -0.99193       -0.014502
v  ǁVelocityǁ             0.010281          19.973          5.9922          7.1158
v  Pressure                 -26714       1.894e+05      1.2401e+05           99491
v  k                    3.2146e-07          4.9358         0.06529         0.10212
v  epsilon               0.0041652      1.1069e+06            1481          54.048
v  TurbVisc             1.6006e-12         0.49487       0.0033124        0.047417
v  CourantNb               0.57989      8.1631e+05          379.11          78.211
v  FourierNb               0.22664      2.3653e+06          218.96          3.4092
v  total_pressure       4.7329e+05       6.894e+05      6.2401e+05      5.9949e+05
v  Local Time Step            0.01        0.088239        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5888      2.9419e+06          598.06           81.62


 TIME FOR THE TIME STEP              691:        0.17807E+03

===============================================================


 INSTANT    0.692000000E+02   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         0.926501311E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889062E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefi------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16214E+02 0.52669E+01
   Friction velocity        uet   :  0.39598E-01 0.56466E+02
   Friction velocity        uk    :  0.45246E-01 0.56466E+02
   Dimensionless distance   yplus :  0.21854E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13138
   Nb of faces within the viscous sub-layer     :      11576
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44902E+01     650   0.24863E+00   0.10832E+02 0.44813E+01 
c  Velocity[X]                                      0.30565E+01 
c  Velocity[Y]                                      0.53400E+01 
c  Velocity[Z]                                      0.24353E+01 
c  Pressure     0.10472E+00     741   0.81356E-02   0.23023E-01 0.28925E-01 
c  k            0.51124E+00     179   0.73496E-04   0.97515E-03 0.15358E+01 
c  epsilon      0.32917E+04     109   0.69364E-03   0.11454E+07 0.17053E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00077077                             8
a  epsilon                 -15.364                            20
a  Local Time Step      1.3957e-08                        281787


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3283          13.589          1.5617         0.37539
v  Velocity[Y]             -10.819          15.785          1.3259         0.89344
v  Velocity[Z]             -17.322           9.486         -1.0196       -0.014342
v  ǁVelocityǁ             0.014342          19.904          6.0638          7.1201
v  Pressure                 -26743      1.8938e+05        1.24e+05           99450
v  k                    3.8602e-07          4.9506         0.06673         0.10202
v  epsilon                0.007158      1.1074e+06          1570.7           54.37
v  TurbVisc             1.4936e-12         0.49487        0.003278        0.047409
v  CourantNb              0.020817      7.1646e+05          382.41          78.309
v  FourierNb               0.22667      2.3653e+06          218.91          3.4072
v  total_pressure       4.7326e+05      6.8938e+05        6.24e+05      5.9945e+05
v  Local Time Step            0.01         0.10677        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               mi------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16214E+02 0.52669E+01
   Friction velocity        uet   :  0.39598E-01 0.56466E+02
   Friction velocity        uk    :  0.45246E-01 0.56466E+02
   Dimensionless distance   yplus :  0.21854E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13138
   Nb of faces within the viscous sub-layer     :      11576
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44902E+01     650   0.24863E+00   0.10832E+02 0.44813E+01 
c  Velocity[X]                                      0.30565E+01 
c  Velocity[Y]                                      0.53400E+01 
c  Velocity[Z]                                      0.24353E+01 
c  Pressure     0.10472E+00     741   0.81356E-02   0.23023E-01 0.28925E-01 
c  k            0.51124E+00     179   0.73496E-04   0.97515E-03 0.15358E+01 
c  epsilon      0.32917E+04     109   0.69364E-03   0.11454E+07 0.17053E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     ----------------------------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16214E+02 0.52669E+01
   Friction velocity        uet   :  0.39598E-01 0.56466E+02
   Friction velocity        uk    :  0.45246E-01 0.56466E+02
   Dimensionless distance   yplus :  0.21854E-02 0.23856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13138
   Nb of faces within the viscous sub-layer     :      11576
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44902E+01     650   0.24863E+00   0.10832E+02 0.44813E+01 
c  Velocity[X]                                      0.30565E+01 
c  Velocity[Y]                                      0.53400E+01 
c  Velocity[Z]                                      0.24353E+01 
c  Pressure     0.10472E+00     741   0.81356E-02   0.23023E-01 0.28925E-01 
c  k            0.51124E+00     179   0.73496E-04   0.97515E-03 0.15358E+01 
c  epsilon      0.32917E+04     109   0.69364E-03   0.11454E+07 0.17053E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00077077                             8
a  epsilon                 -15.364                            20
a  Local Time Step      1.3957e-08                        281787


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3283          13.589          1.5617         0.37539
v  Velocity[Y]             -10.819          15.785          1.3259         0.89344
v  Velocity[Z]             -17.322           9.486         -1.0196       -0.014342
v  ǁVelocityǁ             0.014342          19.904          6.0638          7.1201
v  Pressure                 -26743      1.8938e+05        1.24e+05           99450
v  k                    3.8602e-07          4.9506         0.06673         0.10202
v  epsilon                0.007158      1.1074e+06          1570.7           54.37
v  TurbVisc             1.4936e-12         0.49487        0.003278        0.047409
v  CourantNb              0.020817      7.1646e+05          382.41          78.309
v  FourierNb               0.22667      2.3653e+06          218.91          3.4072
v  total_pressure 
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.664      2.7432e+06          605.93          81.853


 TIME FOR THE TIME STEP              694:        0.19228E+03

===============================================================


 INSTANT    0.695000000E+02   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         0.119849367E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888686E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16419E+02 0.53279E+01
   Friction velocity        uet   :  0.10844E-01 0.57178E+02
   Friction velocity        uk    :  0.10837E-01 0.57178E+02
   Dimensionless distance   yplus :  0.33760E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13028
   Nb of faces within the viscous sub-layer     :      11632
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44870E+01     630   0.24173E+00   0.11544E+02 0.46295E+01 
c  Velocity[X]                                      0.37897E+01 
c  Velocity[Y]                                      0.54595E+01 
c  Velocity[Z]                                      0.22952E+01 
c  Pressure     0.10746E+00     978   0.80581E-02   0.23648E-01 0.59341E-01 
c  k            0.51125E+00     171   0.73695E-04   0.11124E-02 0.16404E+01 
c  epsilon      0.33037E+04     103   0.77948E-03   0.96969E+06 0.15955E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k        
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.664      2.7432e+06          605.93          81.853


 TIME FOR THE TIME STEP              694:        0.18602E+03

===============================================================


 INSTANT    0.695000000E+02   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         0.119849367E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888686E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
----------------------------------------------------------
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.664      2.7432e+06          605.93          81.853


 TIME FOR THE TIME STEP              694:        0.17712E+03

===============================================================


 INSTANT    0.695000000E+02   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         0.119849367E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888686E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16419E+02 0.53279E+01
   Friction velocity        uet   :  0.10844E-01 0.57178E+02
   Friction velocity        uk    :  0.10837E-01 0.57178E+02
   Dimensionless distance   yplus :  0.33760E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13028
   Nb of faces within the viscous sub-layer     :      11632
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44870E+01     630   0.24173E+00   0.11544E+02 0.46295E+01 
c  Velocity[X]                                      0.37897E+01 
c  Velocity[Y]                                      0.54595E+01 
c  Velocity[Z]                                      0.22952E+01 
c  Pressure     0.10746E+00     978   0.80581E-02   0.23648E-01 0.59341E-01 
c  k            0.51125E+00     171   0.73695E-04   0.11124E-02 0.16404E+01 
c  epsilon      0.33037E+04     103   0.77948E-03   0.96969E+06 0.15955E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for a  k                   -0.00043706                             6
a  epsilon                 -85.505                             6
a  Local Time Step      1.4817e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2806          13.431          1.5464         0.37617
v  Velocity[Y]              -10.88          15.175          1.2936         0.89433
v  Velocity[Z]               -17.9          11.416         -1.0247       -0.013579
v  ǁVelocityǁ             0.017494          20.454           6.032          7.1178
v  Pressure                 -26770      1.8936e+05      1.2397e+05           99443
v  k                    3.5429e-07          4.7739         0.06516           0.102
v  epsilon               0.0082729      1.1256e+06          1470.5          53.992
v  TurbVisc             1.0182e-12         0.49487       0.0032716        0.047392
v  CourantNb             0.0082401       6.749e+05          375.86          78.316
v  FourierNb               0.22593      2.3653e+06          218.91          3.4066
v  total_pressure       4.7323e+05      6.8936e+05      6.2397e+05      5.9944e+05
v  Local Time Step            0.01        0.049013            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5992      2.7447e+06          594.77          81.722


 TIME FOR THE TIME STEP              696:        0.18186E+03

===============================================================


 INSTANT    0.697000000E+02   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        -0.198405850E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889050E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16241E+02 0.52669E+01
   Friction velocity        uet   :  0.39458E-01 0.44342E+02
   Friction velocity        uk    :  0.46819E-01 0.44342E+02
   Dimensioa  k                   -0.00043706                             6
a  epsilon                 -85.505                             6
a  Local Time Step      1.4817e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2806          13.431          1.5464         0.37617
v  Velocity[Y]              -10.88          15.175          1.2936         0.89433
v  Velocity[Z]               -17.9          11.416         -1.0247       -0.013579
v  ǁVelocityǁ             0.017494          20.454           6.032          7.1178
v  Pressure                 -26770      1.8936e+05      1.2397e+05           99443
v  k                    3.5429e-07          4.7739         0.06516           0.102
v  epsilon               0.0082729      1.1256e+06          1470.5          53.992
v  TurbVisc             1.0182e-12         0.49487       0.0032716        0.047392
v  CourantNb             0.0082401       6.749e+05          375.86          78.316
v  FourierNb               0.22593      2.3653e+06          218.91          3.4066
v  total_pressure       4.7323e+05      6.8936e+05      6.2397e+05      5.9944e+05
v  Local Time Step            0.01        0.049013            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5a  k                   -0.00043706                             6
a  epsilon                 -85.505                             6
a  Local Time Step      1.4817e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2806          13.431          1.5464         0.37617
v  Velocity[Y]              -10.88          15.175          1.2936         0.89433
v  Velocity[Z]               -17.9          11.416         -1.0247       -0.013579
v  ǁVelocityǁ             0.017494          20.454           6.032          7.1178
v  Pressure                 -26770      1.8936e+05      1.2397e+05           99443
v  k                    3.5429e-07          4.7739         0.06516           0.102
v  epsilon               0.0082729      1.1256e+06          1470.5          53.992
v  TurbVisc             1.0182e-12         0.49487       0.0032716        0.047392
v  CourantNb             0.0082401       6.749e+05          375.86          78.316
v  FourierNb               0.22593      2.3653e+06          218.91          3.4066
v  total_pressure       4.7323e+05      6.8936e+05      6.2397e+05      5.9944e+05
v  Local Time Step            0.01        0.049013            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5992      2.7447e+06          594.77          81.722


 TIME FOR THE TIME STEP              696:        0.17136E+03

===============================================================


 INSTANT    0.697000000E+02   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        -0.198405850E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889050E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
----------------------------------   Dimensionless distance   yplus :  0.84808E-03 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13101
   Nb of faces within the viscous sub-layer     :      11490
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44968E+01     640   0.24250E+00   0.11512E+02 0.46236E+01 
c  Velocity[X]                                      0.27774E+01 
c  Velocity[Y]                                      0.61250E+01 
c  Velocity[Z]                                      0.26095E+01 
c  Pressure     0.10269E+00     904   0.79484E-02   0.22606E-01 0.44396E-01 
c  k            0.51150E+00     156   0.88189E-04   0.11985E-02 0.17020E+01 
c  epsilon      0.33589E+04      95   0.99997E-03   0.15881E+07 0.19900E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                      -0.00302                            38
a  epsilon                 -131.68                            78
a  Local Time Step      1.3105e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5268          13.787          1.5683          0.3744
v  Velocity[Y]             -10.601          15.426          1.3081         0.89367
v  Velocity[Z]              -15.72          9.4722         -1.0081       -0.014889
v  ǁVelocityǁ             0.010368          18.425          6.0081          7.1131
v  Pressure                 -26773      1.8941e+05      1.2403e+05           99505
v  k                    4.0471e-07          4.9555        0.066499         0.10211
v  epsilon               0.0013765      1.1731e+06          1565.8          54.438
v  TurbVisc             1.4907e-12         0.49487       0.0032733        0.047404
v  CourantNb              0.064256      7.6307e+05          386.45          78.473
v  FourierNb               0.22665      2.3653e+06          218.93          3.4079
v  total_pressure       4.7323e+05      6.8941e+05      6.2403e+05      5.9951e+05
v  Local Time Step            0.01        0.059306        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5918      2.8291e+06          605.38          81.881


 TIME FOR THE TIME STEP              698:        0.18827E+03

===============================================================


 INSTANT    0.69   Dimensionless distance   yplus :  0.84808E-03 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13101
   Nb of faces within the viscous sub-layer     :      11490
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44968E+01     640   0.24250E+00   0.11512E+02 0.46236E+01 
c  Velocity[X]                                      0.27774E+01 
c  Velocity[Y]                                      0.61250E+01 
c  Velocity[Z]                                      0.26095E+01 
c  Pressure     0.10269E+00     904   0.79484E-02   0.22606E-01 0.44396E-01 
c  k            0.51150E+00     156   0.88189E-04   0.11985E-02 0.17020E+01 
c  epsilon      0.33589E+04      95   0.99997E-03   0.15881E+07 0.19900E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                      -0.00302                            38
a  epsilon                 -131.68                            78
a  Local Time Step      1.3105e-08                        281785


     Dimensionless distance   yplus :  0.84808E-03 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13101
   Nb of faces within the viscous sub-layer     :      11490
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44968E+01     640   0.24250E+00   0.11512E+02 0.46236E+01 
c  Velocity[X]                                      0.27774E+01 
c  Velocity[Y]                                      0.61250E+01 
c  Velocity[Z]                                      0.26095E+01 
c  Pressure     0.10269E+00     904   0.79484E-02   0.22606E-01 0.44396E-01 
c  k            0.51150E+00     156   0.88189E-04   0.11985E-02 0.17020E+01 
c  epsilon      0.33589E+04      95   0.99997E-03   0.15881E+07 0.19900E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                      -0.00302                            38
a  epsilon                 -131.68                            78
a  Local Time Step      1.3105e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5268          13.787          1.5683          0.3744
v  Velocity[Y]             -10.601          15.426          1.3081         0.89367
v  Velocity[Z]              -15.72          9.4722         -1.0081       -0.014889
v  ǁVelocityǁ             0.010368          18.425          6.0081          7.1131
v  Pressure                 -26773      1.8941e+05      1.2403e+05           99505
v  k                    4.0471e-07          4.9555        0.066499         0.10211
v  epsilon               0.0013765      1.1731e+06          1565.8          54.438
v  TurbVisc             1.4907e-12         0.49487       0.0032733        0.047404
v  CourantNb              0.064256      7.6307e+05          386.45          78.473
v  FourierNb               0.22665      2.3653e+06          218.93          3.4079
v  total_pressure       4.7323e+05      6.8941e+05      6.2403e+05      5.9951e+05
v  Local Time Step            0.01        0.059306        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
    INSTANT    0.700000000E+02   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        -0.672553053E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889058E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15712E+02 0.52990E+01
   Friction velocity        uet   :  0.34177E-01 0.50585E+02
   Friction velocity        uk    :  0.37074E-01 0.50585E+02
   Dimensionless distance   yplus :  0.44340E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13116
   Nb of faces within the viscous sub-layer     :      11656
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44885E+01     635   0.24352E+00   0.97941E+01 0.42640E+01 
c  Velocity[X]                                      0.24420E+01 
c  Velocity[Y]                                      0.49581E+01 
c  Velocity[Z]                                      0.23940E+01 
c  Pressure     0.10671E+00     722   0.81063E-02   0.23538E-01 0.23866E-01 
c  k            0.51142E+00     181   0.85447E-04   0.11081E-02 0.16369E+01 
c  epsilon      0.32703E+04     105   0.80286E-03   0.11428E+07 0.17416E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0065264                            10
a  epsilon                 -555.39                            37
a  Local Time Step      1.4215e-08                        281789


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  INSTANT    0.700000000E+02   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        -0.672553053E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889058E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15712E+02 0.52990E+01
   Friction velocity        uet   :  0.34177E-01 0.50585E+02
   Friction velocity        uk    :  0.37074E-01 0.50585E+02
   Dimensionless distance   yplus :  0.44340E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13116
   Nb of faces INSTANT    0.700000000E+02   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        -0.672553053E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312889058E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15712E+02 0.52990E+01
   Friction velocity        uet   :  0.34177E-01 0.50585E+02
   Friction velocity        uk    :  0.37074E-01 0.50585E+02
   Dimensionless distance   yplus :  0.44340E-02 0.23857E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13116
   Nb of faces within the viscous sub-layer     :      11656
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44885E+01     635   0.24352E+00   0.97941E+01 0.42640E+01 
c  Velocity[X]                                      0.24420E+01 
c  Velocity[Y]                                      0.49581E+01 
c  Velocity[Z]                                      0.23940E+01 
c  Pressure     0.10671E+00     722   0.81063E-02   0.23538E-01 0.23866E-01 
c  k            0.51142E+00     181   0.85447E-04   0.11081E-02 0.16369E+01 
c  epsilon      0.32703E+04     105   0.80286E-03   0.11428E+07 0.17416E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0065264                            10
a  epsilon                 -555.39                            37
a-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4755          13.855          1.6105         0.38823
v  Velocity[Y]             -11.026          16.957          1.3937         0.92132
v  Velocity[Z]             -14.965          10.339         -1.0281     -0.00052909
v  ǁVelocityǁ            0.0092033          19.872          6.1443          7.3408
v  Pressure                 -23070      1.9424e+05      1.2881e+05      1.0408e+05
v  k                     4.962e-07          4.8958        0.067211         0.10841
v  epsilon                0.006243      1.0921e+06          1575.9          55.506
v  TurbVisc             1.5127e-12         0.49487        0.003263         0.04741
v  CourantNb               0.10615      7.7601e+05          382.42          78.349
v  FourierNb               0.22731      2.3653e+06           218.9          3.4064
v  total_pressure       4.7693e+05      6.9424e+05      6.2881e+05      6.0408e+05
v  Local Time Step            0.01        0.076557        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5841      2.7276e+06          601.32          81.755


 TIME FOR THE TIME STEP              701:        0.23429E+03

===============================================================


 INSTANT    0.702000000E+02   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         0.184731184E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160418E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16426E+02 0.55361E+01
   Friction velocity        uet   :  0.23564E-01 0.44368E+02
   Friction velocity        uk    :  0.23311E-01 0.44368E+02
   Dimensionless distance   yplus :  0.24068E-02 0.24772E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13256
   Nb of faces within the viscous sub-layer     :      11473
   Total number of wall faces                   :      41000
---------------------------------------------------  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4755          13.855          1.6105         0.38823
v  Velocity[Y]             -11.026          16.957          1.3937         0.92132
v  Velocity[Z]             -14.965          10.339         -1.0281     -0.00052909
v  ǁVelocityǁ            0.0092033          19.872          6.1443          7.3408
v  Pressure                 -23070      1.9424e+05      1.2881e+05      1.0408e+05
v  k                     4.962e-07          4.8958        0.067211         0.10841
v  epsilon                0.006243      1.0921e+06          1575.9          55.506
v  TurbVisc             1.5127e-12         0.49487        0.003263         0.04741
v  CourantNb               0.10615      7.7601e+05          382.42          78.349
v  FourierNb               0.22731      2.3653e+06           218.9          3.4064
v  total_pressure       4.7693e+05      6.9424e+05      6.2881e+05      6.0408e+05
v  Local Time Step            0.01        0.076557        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5841      2.7276e+06          601.32          81.755


 TIME FOR THE TIME STEP              701:        0.23944E+03

===============================================================


 INSTANT    0.702000000E+02   TIME STEP NUMBER             702
 ============================================================= 




   ** BOUNDARY MASS FLOW INF-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4755          13.855          1.6105         0.38823
v  Velocity[Y]             -11.026          16.957          1.3937         0.92132
v  Velocity[Z]             -14.965          10.339         -1.0281     -0.00052909
v  ǁVelocityǁ            0.0092033          19.872          6.1443          7.3408
v  Pressure                 -23070      1.9424e+05      1.2881e+05      1.0408e+05
v  k                     4.962e-07          4.8958        0.067211         0.10841
v  epsilon                0.006243      1.0921e+06          1575.9          55.506
v  TurbVisc             1.5127e-12         0.49487        0.003263         0.04741
v  CourantNb               0.10615      7.7601e+05          382.42          78.349
v  FourierNb               0.22731      2.3653e+06           218.9          3.4064
v  total_pressure       4.7693e+05      6.9424e+05      6.2881e+05      6.0408e+05
v  Local Time Step            0.01        0.076557        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5841      2.7276e+06          601.32          81.755


 TIME FOR THE TIME STEP              701:        0.24366E+03

===============================================================


 INSTANT    0.702000000E+02   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         0.184731184E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160418E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16426E+02 0.55361E+01
   Friction velocity        uet   :  0.23564E-01 0.44368E+02
   Friction velocity        uk    :  0.23311E-01 0.44368E+02
   Dimensionless distance   yplus :  0.24068E-02 0.24772E+02
   ----------------------------------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48633E+01     784   0.22994E+00   0.10582E+02 0.42611E+01 
c  Velocity[X]                                      0.28915E+01 
c  Velocity[Y]                                      0.52705E+01 
c  Velocity[Z]                                      0.24201E+01 
c  Pressure     0.13408E+00    1330   0.17101E-01   0.29403E-01 0.62134E+00 
c  k            0.57881E+00     273   0.13083E-03   0.21213E-02 0.20862E+01 
c  epsilon      0.34764E+04     158   0.11154E-02   0.17696E+07 0.20745E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0060712                            20
a  epsilon                 -236.53                            63
a  Local Time Step      1.3636e-08                        281789


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3535          13.389          1.6157         0.39483
v  Velocity[Y]             -11.165          17.357          1.3614         0.94179
v  Velocity[Z]             -15.753          11.321         -0.9582         0.02042
v  ǁVelocityǁ             0.025196          20.243          6.0953          7.4114
v  Pressure                 -22189      1.9944e+05      1.3301e+05      1.0665e+05
v  k                    1.3758e-07          5.0315        0.067268         0.11066
v  epsilon              0.00032676      1.1551e+06          1588.1          56.759
v  TurbVisc             1.6941e-12         0.51512       0.0034647          0.0504
v  CourantNb              0.066593      7.3334e+05          390.35            80.9
v  FourierNb               0.22701      2.3653e+06          218.96          3.4551
v  total_pressure       4.7781e+05      6.9944e+05      6.3301e+05      6.0665e+05
v  Local Time Step            0.01        0.026169            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5716      2.8537e+06          609.31          84.355


 TIME FOR THE TIME STEP              703:        0.21507E+03

===============================================================


 INSTANT    0.704000000E+02   TIME STEP NUMBER             704
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces         ------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48633E+01     784   0.22994E+00   0.10582E+02 0.42611E+01 
c  Velocity[X]                                      0.28915E+01 
c  Velocity[Y]                                      0.52705E+01 
c  Velocity[Z]                                      0.24201E+01 
c  Pressure     0.13408E+00    1330   0.17101E-01   0.29403E-01 0.62134E+00 
c  k            0.57881E+00     273   0.13083E-03   0.21213E-02 0.20862E+01 
c  epsilon      0.34764E+04     158   0.11154E-02   0.17696E+07 0.20745E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0060712                            20
a  epsilon                 -236.53                            63
a  Local Time Step      1.3636e-08                        281789


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3535          13.389          1.6157         0.------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48633E+01     784   0.22994E+00   0.10582E+02 0.42611E+01 
c  Velocity[X]                                      0.28915E+01 
c  Velocity[Y]                                      0.52705E+01 
c  Velocity[Z]                                      0.24201E+01 
c  Pressure     0.13408E+00    1330   0.17101E-01   0.29403E-01 0.62134E+00 
c  k            0.57881E+00     273   0.13083E-03   0.21213E-02 0.20862E+01 
c  epsilon      0.34764E+04     158   0.11154E-02   0.17696E+07 0.20745E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0060712                            20
a  epsilon                 -236.53                            63
a  Local Time Step      1.3636e-08                        281789


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3535          13.389          1.6157         0.39483
v  Velocity[Y]             -11.165          17.357          1.3614         0.94179
v  Velocity[Z]             -15.753          11.321         -0.9582         0.02042
v  ǁVelocityǁ             0.025196          20.243          6.0953          7.4114
v  Pressure                 -22189      1.9944e+05      1.3301e+05      1.0665e+05
v  k                    1.3758e-07          5.0315        0.067268         0.11066
v  epsilon              0.00032676      1.1551e+06          1588.1          56.759
v  TurbVisc             1.6941e-12         0.51512       0.0034647          0.0504
v  CourantNb              0.066593      7.3334e+05          390.35            80.9
v  FourierNb               0.22701      2.3653e+06          218.96          3.4551
v  total_pressure       4.7781e+05      6.9944e+05      6.3301e+05      6.0665e+05
v  Local Time Step            0.01        0.026169            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5716      2.8537e+06          609.31          84.355


 TIME FOR THE TIME STEP              703:        0.23013E+03

===============================================================


 INSTANT    0.704000000E+02   TIME STEP NUMBER             7Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.148596431E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160850E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16670E+02 0.55416E+01
   Friction velocity        uet   :  0.41749E-01 0.47756E+02
   Friction velocity        uk    :  0.47945E-01 0.47756E+02
   Dimensionless distance   yplus :  0.60937E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13327
   Nb of faces within the viscous sub-layer     :      11433
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48637E+01     739   0.23390E+00   0.10926E+02 0.43162E+01 
c  Velocity[X]                                      0.29297E+01 
c  Velocity[Y]                                      0.57440E+01 
c  Velocity[Z]                                      0.22527E+01 
c  Pressure     0.13378E+00    1341   0.15187E-01   0.29187E-01 0.87293E+00 
c  k            0.57885E+00     229   0.73438E-04   0.10193E-02 0.14442E+01 
c  epsilon      0.33983E+04     124   0.71178E-03   0.10363E+07 0.15984E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0023907                            40
a  epsilon                 -28.159                            51
a  Local Time Step      1.2576e-08                        281786


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5404          13.564          1.6171         0.39088
v  Velocity[Y]             -10.781          16.522          1.4345         0.93474
v  Velocity[Z]             -14.703          10.397         -1.0602      Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.148596431E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160850E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16670E+02 0.55416E+01
   Friction velocity        uet   :  0.41749E-01 0.47756E+02
   Friction velocity        uk    :  0.47945E-01 0.47756E+02
   Dimensionless distance   yplus :  0.60937E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13327
   Nb of faces within the viscous sub-layer     :      11433
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
--------------------------------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.148596431E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160850E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16670E+02 0.55416E+01
   Friction velocity        uet   :  0.41749E-01 0.47756E+02
   Friction velocity        uk    :  0.47945E-01 0.47756E+02
   Dimensionless distance   yplus :  0.60937E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13327
   Nb of faces within the viscous sub-layer     :      11433
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48637E+01     739   0.23390E+00   0.10926E+02 0.43162E+01 
c  Velocity[X]                                      0.29297E+01 
c  Velocity[Y]                                      0.57440E+01 
c  Velocity[Z]                                      0.22527E+01 
c  Pressure     0.13378E+00    1341   0.15187E-01   0.29187E-01 0.87293E+00 
c  k            0.57885E+00     229   0.73438E-04   0.10193E-02 0.14442E+01 
c  epsilon      0.33983E+04     124   0.71178E-03   0.10363E+07 0.15984E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0023907                            40
a  epsilon                 -28.159                            51
a  Local Time Step      1.2576e-08                        281786


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  ---v  Velocity[Z]             -14.328          9.7577         -1.0588       -0.021321
v  ǁVelocityǁ             0.026324          18.853          6.1778          7.4269
v  Pressure                 -27066      1.9806e+05      1.3042e+05       1.041e+05
v  k                    3.9096e-07          4.9315        0.068563         0.11085
v  epsilon                0.001549      1.1631e+06          1633.7          57.368
v  TurbVisc             7.9295e-13          0.5151       0.0035287        0.050315
v  CourantNb              0.046893      8.0853e+05          392.99          81.291
v  FourierNb               0.22717      2.3653e+06          218.97          3.4596
v  total_pressure       4.7293e+05      6.9806e+05      6.3042e+05       6.041e+05
v  Local Time Step            0.01        0.026027            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6956      2.9341e+06          611.96          84.751


 TIME FOR THE TIME STEP              706:        0.20636E+03

===============================================================


 INSTANT    0.707000000E+02   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         0.935058648E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160830E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16598E+02 0.55416E+01
   Friction velocity        uet   :  0.40056E-01 0.29440E+02
   Friction velocity        uk    :  0.42874E-01 0.29440E+02
   Dimensionless distance   yplus :  0.34612E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13415
   Nb of faces within the viscous sub-layer     :      11420
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-------------v  Velocity[Z]             -14.328          9.7577         -1.0588       -0.021321
v  ǁVelocityǁ             0.026324          18.853          6.1778          7.4269
v  Pressure                 -27066      1.9806e+05      1.3042e+05       1.041e+05
v  k                    3.9096e-07          4.9315        0.068563         0.11085
v  epsilon                0.001549      1.1631e+06          1633.7          57.368
v  TurbVisc             7.9295e-13          0.5151       0.0035287        0.050315
v  CourantNb              0.046893      8.0853e+05          392.99          81.291
v  FourierNb               0.22717      2.3653e+06          218.97          3.4596
v  total_pressure       4.7293e+05      6.9806e+05      6.3042e+05       6.041e+05
v  Local Time Step            0.01        0.026027            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6956      2.9341e+06          611.96          84.751


 TIME FOR THE TIME STEP              706:        0.20630E+03

===============================================================


 INSTANT    0.707000000E+02   TIME STEP NUMBER             707
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet         v  Velocity[Z]             -14.328          9.7577         -1.0588       -0.021321
v  ǁVelocityǁ             0.026324          18.853          6.1778          7.4269
v  Pressure                 -27066      1.9806e+05      1.3042e+05       1.041e+05
v  k                    3.9096e-07          4.9315        0.068563         0.11085
v  epsilon                0.001549      1.1631e+06          1633.7          57.368
v  TurbVisc             7.9295e-13          0.5151       0.0035287        0.050315
v  CourantNb              0.046893      8.0853e+05          392.99          81.291
v  FourierNb               0.22717      2.3653e+06          218.97          3.4596
v  total_pressure       4.7293e+05      6.9806e+05      6.3042e+05       6.041e+05
v  Local Time Step            0.01        0.026027            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6956      2.9341e+06          611.96          84.751


 TIME FOR THE TIME STEP              706:        0.21815E+03

===============================================================


 INSTANT    0.707000000E+02   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         0.935058648E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160830E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16598E+02 0.55416E+01
   Friction velocity        uet   :  0.40056E-01 0.29440E+02
   Friction velocity        uk    :  0.42874E-01 0.29440E+02
   Dimensionless distance   yplus :  0.34612E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13415
   Nb of faces within the viscous sub-layer     :      11420
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48630E+01     692   0.23609E+00   0.11708E+02 0.44701E+01 
c  Velocity[X]                                      0.31864E+01 
c  Velocity[Y]                                      0.61211E+01 
c  Velocity[Z]                                      0.24003E+01 
c  Pressure     0.12880E+00    1234   0.13285E-01   0.27974E-01 0.32694E+00 
c  k            0.57889E+00     192   0.56819E-04   0.91648E-03 0.13693E+01 
c  epsilon      0.35294E+04     102   0.10859E-02   0.10474E+07 0.15528E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00020613                            13
a  epsilon                 -29.296                            20
a  Local Time Step      1.3947e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3324          13.629          1.6219         0.39011
v  Velocity[Y]             -11.114          16.484          1.3605         0.93492
v  Velocity[Z]               -14.7          11.379         -1.0509       -0.020158
v  ǁVelocityǁ             0.023333          19.425          6.1505          7.4286
v  Pressure                 -27918      1.9777e+05      1.2987e+05      1.0376e+05
v  k                    2.6105e-07           5.104        0.068746         0.11089
v  epsilon               0.0031146      1.1771e+06          1648.6          57.545
v  TurbVisc             1.6153e-12          0.5151       0.0035514        0.050317
v  CourantNb             0.0010273      7.1698e+05          393.16          81.257
v  FourierNb               0.22692      2.3653e+06             219          3.4621
v  total_pressure       4.7208e+05      6.9777e+05      6.2987e+05      6.0376e+05
v  Local Time Step            0.01        0.028629            0.01        0.010002


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.721      2.7756e+06          612.16          84.719


 TIME FOR THE TIME STEP              707:        0.20491E+03

===============================================================


 INSTANT    0.708000000E+02   TIME STEP NUMBER             708
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
-----------------------------------------------------------------------------
c  Velocity     0.48620E+01     686   0.23632E+00   0.91201E+01 0.39488E+01 
c  Velocity[X]                                      0.24086E+01 
c  Velocity[Y]                                      0.43768E+01 
c  Velocity[Z]                                      0.23346E+01 
c  Pressure     0.12847E+00    1123   0.13329E-01   0.27832E-01 0.16003E+00 
c  k            0.57890E+00     172   0.63690E-04   0.94325E-03 0.13892E+01 
c  epsilon      0.34719E+04     107   0.78505E-03   0.13614E+07 0.18284E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.009122                            23
a  epsilon                 -667.14                            44
a  Local Time Step      1.3123e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6265          13.612          1.6293         0.39029
v  Velocity[Y]              -11.22          16.321          1.3727         0.93529
v  Velocity[Z]             -15.122          11.104         -1.0479       -0.016468
v  ǁVelocityǁ             0.024996          19.328          6.1719          7.4213
v  Pressure                 ------------------------------------------------------------------------------
c  Velocity     0.48620E+01     686   0.23632E+00   0.91201E+01 0.39488E+01 
c  Velocity[X]                                      0.24086E+01 
c  Velocity[Y]                                      0.43768E+01 
c  Velocity[Z]                                      0.23346E+01 
c  Pressure     0.12847E+00    1123   0.13329E-01   0.27832E-01 0.16003E+00 
c  k            0.57890E+00     172   0.63690E-04   0.94325E-03 0.13892E+01 
c  epsilon      0.34719E+04     107   0.78505E-03   0.13614E+07 0.18284E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.009122                            23
a  epsilon                 -667.14                            44
a  Local Time Step      1.3123e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6265          13.612          1.6293         0.39029
v  Velocity[Y]              -11.22          16.321          1.3727         0.93529
v  Velocity[Z]             -15.122          11.104         -1.0479       -0.016468
v  ǁVelocityǁ             0.024996          19.328          6.1719          7.4213
v  Pressure                 -28323      1.9775e+05      1.2963e+05       1.037e+05
v  k                    4.1183e-07           4.844        0.068362         0.11089
v  epsilon               0.0019701      1.1491e+06          1592.4          57.465
v  TurbVisc             1.4358e-12          0.5151       0.0035641        0.050321
v  CourantNb               0.44733        7.62e+05          388.35          81.326
v  FourierNb               0.22679      2.3653e+06          219.01          3.4634
v  total_pressure       4.7168e+05      6.9775e+05      6.2963e+05       6.037e+05
v  Local Time Step            0.01        0.031492            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.633       2.603e+06          607.36          84.789


 TIME FOR THE TIME STEP              708:        0.19022E+03

===============================================================


 INSTANT    0.709000000E+02   TIME STEP NUMBER             709
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
----------------------------------------------Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160442E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16588E+02 0.55413E+01
   Friction velocity        uet   :  0.38008E-01 0.47937E+02
   Friction velocity        uk    :  0.40623E-01 0.47937E+02
   Dimensionless distance   yplus :  0.53888E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13418
   Nb of faces within the viscous sub-layer     :      11385
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48632E+01     632   0.23788E+00   0.11757E+02 0.44825E+01 
c  Velocity[X]                                      0.32661E+01 
c  Velocity[Y]                                      0.59467E+01 
c  Velocity[Z]                                      0.25443E+01 
c  Pressure     0.12610E+00    1196   0.12123E-01   0.27196E-01 0.33545E+00 
c  k            0.57900E+00     179   0.62947E-04   0.88504E-03 0.13451E+01 
c  epsilon      0.34512E+04     101   0.70103E-03   0.78974E+06 0.13820E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.001134                            14
a  epsilon                 -140.53                            26
a  Local Time Step       1.282e-08                        281776


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6299          13.738          1.6305         0.39108
v  Velocity[Y]             -10.838          15.736          1.3846         0.93522
v  Velocity[Z]             -14.252          11.667         -1.0226       -0.013634
v  ǁVelocityǁ             0.014639          18.626          6.2111          7.4221
v  Pressure                 -28238      1.9852e+05      1.3007e+05      1.0429e+05
v  k                    3.9215e-07           4.863        0.069336         0.11103
v  epsilon               0.0010539      1.1352e+06    Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160442E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16588E+02 0.55413E+01
   Friction velocity        uet   :  0.38008E-01 0.47937E+02
   Friction velocity        uk    :  0.40623E-01 0.47937E+02
   Dimensionless distance   yplus :  0.53888E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13418
   Nb of faces within the viscous sub-layer     :      11385
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48632E+01     632   0.23788E+00   0.11757E+02 0.44825E+01 
c  Velocity[X]                       Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160442E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16588E+02 0.55413E+01
   Friction velocity        uet   :  0.38008E-01 0.47937E+02
   Friction velocity        uk    :  0.40623E-01 0.47937E+02
   Dimensionless distance   yplus :  0.53888E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13418
   Nb of faces within the viscous sub-layer     :      11385
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48632E+01     632   0.23788E+00   0.11757E+02 0.44825E+01 
c  Velocity[X]                                      0.32661E+01 
c  Velocity[Y]                                      0.59467E+01 
c  Velocity[Z]                                      0.25443E+01 
c  Pressure     0.12610E+00    1196   0.12123E-01   0.27196E-01 0.33545E+00 
c  k            0.57900E+00     179   0.62947E-04   0.88504E-03 0.13451E+01 
c  epsilon      0.34512E+04     101   0.70103E-03   0.78974E+06 0.13820E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.001134                            14
a  epsilon                 -140.53                            26
a  Local Time Step       1.282e-08                        281776


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6299          13.738          1.6305         0.39108
v  Velocity[Y]             -10.838          15.736          1.3846         0.93522
v  Velocity[Z]             -14.252          11.667         -1.0226       -0.013634
v  ǁVelocityǁ             0.014639     v  epsilon               0.0053699      1.1589e+06          1639.6          57.793
v  TurbVisc             1.6012e-12          0.5151       0.0035638         0.05034
v  CourantNb               0.39903      7.1289e+05          395.19           81.44
v  FourierNb               0.22731      2.3653e+06          219.01          3.4619
v  total_pressure       4.7204e+05      6.9909e+05      6.3051e+05      6.0473e+05
v  Local Time Step            0.01        0.031649            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7252      2.7295e+06          614.19          84.902


 TIME FOR THE TIME STEP              711:        0.20801E+03

===============================================================


 INSTANT    0.712000000E+02   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         0.220924061E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160417E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16702E+02 0.55413E+01
   Friction velocity        uet   :  0.39842E-01 0.58505E+02
   Friction velocity        uk    :  0.42695E-01 0.58505E+02
   Dimensionless distance   yplus :  0.51399E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13359
   Nb of faces within the viscous sub-layer     :      11351
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48720E+01     627   0.23866E+00   0.10218E+02 0.41788E+01 
c  Velocity[X]                                      0.29543E+01 
c  Velocity[Y]                                      0.47462E+01 
c  Velocity[Z]                                      0.25176E+0v  epsilon               0.0053699      1.1589e+06          1639.6          57.793
v  TurbVisc             1.6012e-12          0.5151       0.0035638         0.05034
v  CourantNb               0.39903      7.1289e+05          395.19           81.44
v  FourierNb               0.22731      2.3653e+06          219.01          3.4619
v  total_pressure       4.7204e+05      6.9909e+05      6.3051e+05      6.0473e+05
v  Local Time Step            0.01        0.031649            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7252      2.7295e+06          614.19          84.902


 TIME FOR THE TIME STEP              711:        0.19359E+03

===============================================================


 INSTANT    0.712000000E+02   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         0.220924061E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160417E+01
Free inlet               13 v  epsilon               0.0053699      1.1589e+06          1639.6          57.793
v  TurbVisc             1.6012e-12          0.5151       0.0035638         0.05034
v  CourantNb               0.39903      7.1289e+05          395.19           81.44
v  FourierNb               0.22731      2.3653e+06          219.01          3.4619
v  total_pressure       4.7204e+05      6.9909e+05      6.3051e+05      6.0473e+05
v  Local Time Step            0.01        0.031649            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7252      2.7295e+06          614.19          84.902


 TIME FOR THE TIME STEP              711:        0.19871E+03

===============================================================


 INSTANT    0.712000000E+02   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         0.220924061E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160417E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16702E+02 0.55413E+01
   Friction velocity        uet   :  0.39842E-01 0.58505E+02
   Friction velocity        uk    :  0.42695E-01 0.58505E+02
   Dimensionless distance   yplus :  0.51399E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13359
   Nb of faces within the viscous sub-layer     :      11351
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48720E+01     627   0.23866E+00   0.10218E+02 0.41788E+01 
c  Velocity[X]                                      0.29543E+01 
c  Velocity[Y]                                      0.47462E+01 
c  Velocity[Z]                                      0.25176E+01 
c  Pressure     0.12093E+00    1194   0.11604E-01   0.25957E-01 0.29955E+00 
c  k            0.57905E+00     163   0.58143E-04   0.87148E-03 0.13347E+01 
c  epsilon      0.34660E+04     113   0.50121E-03   0.85656E+06 0.14398E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00062513                             7
a  epsilon                 -92.375                            14
a  Local Time Step      1.2866e-08                        281778


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6196          13.702          1.6517         0.39286
v  Velocity[Y]             -11.366          16.718          1.3487         0.93802
v  Velocity[Z]             -13.873          10.636        -0.99812       -0.012852
v  ǁVelocityǁ             0.011027          19.671           6.163          7.4215
v  Pressure                 -27636      1.9957e+05      1.3089e+05       1.051e+05
v  k                    4.8252e-07          4.8786        0.068834         0.11116
v  epsilon                0.004589      1.1779e+06            1598           57.77
v  TurbVisc             1.2778e-13          0.5151       0.0035781        0.050353
v  CourantNb               0.16191      7.7724e+05          391.06          81.327
v  FourierNb               0.22767      2.3653e+06          219.02          3.4642
v  total_pressure       4.7236e+05      6.9957e+05      6.3089e+05       6.051e+05
v  Local Time Step            0.01        0.032002            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7505      2.6244e+06          610.07          84.792


 TIME FOR THE TIME STEP              712:        0.18744E+03

===============================================================


 INSTANT    0.713000000E+02   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         0.219474353E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3  c  Velocity[Z]                                      0.22288E+01 
c  Pressure     0.12113E+00    1194   0.11204E-01   0.25931E-01 0.28901E+00 
c  k            0.57901E+00     155   0.68644E-04   0.96061E-03 0.14014E+01 
c  epsilon      0.33754E+04     101   0.56200E-03   0.74169E+06 0.13790E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00039395                            31
a  epsilon                 -128.15                            51
a  Local Time Step      1.2783e-08                        281787


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4821          13.824           1.651         0.39343
v  Velocity[Y]             -10.915          15.931          1.3684         0.93766
v  Velocity[Z]             -13.946          11.021         -1.0205        -0.01275
v  ǁVelocityǁ             0.016447          18.849          6.1711          7.4294
v  Pressure                 -27367      2.0003e+05      1.3128e+05      1.0545e+05
v  k                    9.1396e-08          4.8737        0.068397         0.11116
v  epsilon               0.0009425      1.0944e+06          1551.3          57.712
v  TurbVisc             1.4017e-12          0.5151       0.003569c  Velocity[Z]                                      0.22288E+01 
c  Pressure     0.12113E+00    1194   0.11204E-01   0.25931E-01 0.28901E+00 
c  k            0.57901E+00     155   0.68644E-04   0.96061E-03 0.14014E+01 
c  epsilon      0.33754E+04     101   0.56200E-03   0.74169E+06 0.13790E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00039395                            31
a  epsilon                 -128.15                            51
a  Local Time Step      1.2783e-08                        281787


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4821          13.824           1.651         0.39343
v  Velocity[Y]             -10.915          15.931          1.3684         0.93766
v  Velocity[Z]             -13.946          11.021         -1.0205        -0.01275
v  ǁVelocityǁ             0.016447          18.849          6.1711          7.4294
v  Pressure                 -27367      2.0003e+05      1.3128e+05      1.0545e+05
v  k                    9.1396e-08          4.8737        0.068397         0.11116
v  epsilon               0.0009425      1.0944e+06          1551.3          57.712
v  TurbVisc             1.4017e-12          0.5151       0.0035698        0.050357
v  CourantNb              0.051316      7.8231e+05          388.52          81.379
v  FourierNb               0.22778      2.3653e+06             219          3.4638
v  total_pressure       4.7263e+05      7.0003e+05      6.3128e+05      6.0545e+05
v  Local Time Step            0.01        0.035202            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6999      2.7125e+06          607.52          84.843


 TIME FOR THE TIME STEP              713:        0.19335E+03

===============================================================


 INSTANT    0.714000000E+02   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         0.313365629E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0       Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16777E+02 0.55412E+01
   Friction velocity        uet   :  0.33044E-01 0.36734E+02
   Friction velocity        uk    :  0.49233E-01 0.36734E+02
   Dimensionless distance   yplus :  0.28220E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13443
   Nb of faces within the viscous sub-layer     :      11388
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48746E+01     641   0.23740E+00   0.12495E+02 0.46141E+01 
c  Velocity[X]                                      0.30275E+01 
c  Velocity[Y]                                      0.69865E+01 
c  Velocity[Z]                                      0.24807E+01 
c  Pressure     0.12094E+00    1189   0.10367E-01   0.25760E-01 0.22968E+00 
c  k            0.57900E+00     160   0.60126E-04   0.85213E-03 0.13199E+01 
c  epsilon      0.35488E+04      96   0.11280E-02   0.10503E+07 0.15523E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00017605                             4
a  epsilon                  -23.86                            11
a  Local Time Step      1.3757e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4937          13.898          1.6295         0.39477
v  Velocity[Y]             -11.186          16.005          1.3483         0.93974
v  Velocity[Z]             -16.356           11.41         -1.0432       -0.014848
v  ǁVelocityǁ              0.01469          19.098           6.182          7.4289
v  Pressure                 -27031      2.0093e+05      1.3201e+05      1.0602e+05
v  k                    2.7758e-07          5.1436        0.069125         0.11116
v  epsilon               0.0016291      1.1746e+06          1646.5          57.879
v  TurbVisc             1.5527e-12          0.5151       0.0035629        0.050357
v  CourantNb               0.16943      7.2688e+05          393.33          81.587
v  FourierNb               0.22778      2.3653e+06          2Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16777E+02 0.55412E+01
   Friction velocity        uet   :  0.33044E-01 0.36734E+02
   Friction velocity        uk    :  0.49233E-01 0.36734E+02
   Dimensionless distance   yplus :  0.28220E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13443
   Nb of faces within the viscous sub-layer     :      11388
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48746E+01     641   0.23740E+00   0.12495E+02 0.46141E+01 
c  Velocity[X]                                      0.30275E+01 
c  Velocity[Y]                                      0.69865E+01 
c  Velocity[Z]                                      0.24807E+01 
c  Pressure     0.12094E+00    1189   0.10367E-01   0.25760E-01 0.22968E+00 
c  k            0.579Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16777E+02 0.55412E+01
   Friction velocity        uet   :  0.33044E-01 0.36734E+02
   Friction velocity        uk    :  0.49233E-01 0.36734E+02
   Dimensionless distance   yplus :  0.28220E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13443
   Nb of faces within the viscous sub-layer     :      11388
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48746E+01     641   0.23740E+00   0.12495E+02 0.46141E+01 
c  Velocity[X]                                      0.30275E+01 
c  Velocity[Y]                                      0.69865E+01 
c  Velocity[Z]                                      0.24807E+01 
c  Pressure     0.12094E+00    1189   0.10367E-01   0.25760E-01 0.22968E+00 
c  k            0.57900E+00     160   0.60126E-04   0.85213E-03 0.13199E+01 
c  epsilon      0.35488E+04      96   0.11280E-02   0.10503E+07 0.15523E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00017605                             4
a  epsilon                  -23.86                            11
a  Local Time Step      1.3757e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4937          13.898          1.6295         0.39477
v  Velocity[Y]             -11.186          16.005          1.3483         0.93974
v  Velocity[Z]             -16.356           11.41         -1.0432       -0.014848
v  ǁVelocityǁ              0.01469          19.098           6.182          7.4289
v  Pressure                 -27031      2.0093e+05      1.3201e+05      1.0602e+05
v  k                    2.7758e-07          5.1436        0.069125         0.11116
v  epsilon               0.0016291     v  FourierNb               0.22767      2.3653e+06          219.02           3.464
v  total_pressure       4.7305e+05      7.0113e+05      6.3215e+05      6.0612e+05
v  Local Time Step            0.01        0.039049            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.618      2.6783e+06          610.21          84.873


 TIME FOR THE TIME STEP              716:        0.18372E+03

===============================================================


 INSTANT    0.717000000E+02   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         0.119128232E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160434E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16994E+02 0.55412E+01
   Friction velocity        uet   :  0.35712E-01 0.34406E+02
   Friction velocity        uk    :  0.37517E-01 0.34406E+02
   Dimensionless distance   yplus :  0.38794E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13410
   Nb of faces within the viscous sub-layer     :      11380
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48763E+01     621   0.23780E+00   0.10747E+02 0.42754E+01 
c  Velocity[X]                                      0.28869E+01 
c  Velocity[Y]                                      0.50850E+01 
c  Velocity[Z]                                      0.27747E+01 
c  Pressure     0.12142E+00    1030   0.10398E-01   0.25726E-01 0.12280E+00 
c  k            0.57888E+00     164   0.72516E-04   0.10719E-02 0.14805E+01 
c  epsilon      0.34366E+04      99   0.59536E-03   0.13125E+07 0.18162E+02 
---------------v  FourierNb               0.22767      2.3653e+06          219.02           3.464
v  total_pressure       4.7305e+05      7.0113e+05      6.3215e+05      6.0612e+05
v  Local Time Step            0.01        0.039049            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.618      2.6783e+06          610.21          84.873


 TIME FOR THE TIME STEP              716:        0.18359E+03

===============================================================


 INSTANT    0.717000000E+02   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         0.119128232E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160434E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------v  FourierNb               0.22767      2.3653e+06          219.02           3.464
v  total_pressure       4.7305e+05      7.0113e+05      6.3215e+05      6.0612e+05
v  Local Time Step            0.01        0.039049            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.618      2.6783e+06          610.21          84.873


 TIME FOR THE TIME STEP              716:        0.18525E+03

===============================================================


 INSTANT    0.717000000E+02   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         0.119128232E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160434E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16994E+02 0.55412E+01
   Friction velocity        uet   :  0.35712E-01 0.34406E+02
   Friction velocity        uk    :  0.37517E-01 0.34406E+02
   Dimensionless distance   yplus :  0.38794E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13410
   Nb of faces within the viscous sub-layer     :      11380
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48763E+01     621   0.23780E+00   0.10747E+02 0.42754E+01 
c  Velocity[X]                                      0.28869E+01 
c  Velocity[Y]                                      0.50850E+01 
c  Velocity[Z]                                      0.27747E+01 
c  Pressure     0.12142E+00    1030   0.10398E-01   0.25726E-01 0.12280E+00 
c  k            0.57888E+00     164   0.72516E-04   0.10719E-02 0.14805E+01 
c  epsilon      0.34366E+04      99   0.59536E-03   0.13125E+07 0.18162E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0031009                            49
a  epsilon                 -223.04                            87
a  Local Time Step      1.2842e-08                        281779


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4498          13.808          1.6487         0.39428
v  Velocity[Y]             -11.024          15.871          1.3423         0.93977
v  Velocity[Z]             -18.813           9.653         -1.0422       -0.015451
v  ǁVelocityǁ              0.03011          21.345          6.1796          7.4373
v  Pressure                 -26962       2.013e+05      1.3226e+05      1.0621e+05
v  k                    4.6578e-07          4.8987        0.068606         0.11107
v  epsilon               0.0021046      1.1128e+06          1568.5          57.759
v  TurbVisc             1.5943e-12          0.5151       0.0035741        0.050348
v  CourantNb              0.017943      7.7872e+05          388.12          81.548
v  FourierNb               0.22734      2.3653e+06          219.01          3.4641
v  total_pressure       4.7304e+05       7.013e+05      6.3226e+05      6.0621e+05
v  Local Time Step            0.01        0.042954            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6226      2.8243e+06          607.13          85.012


 TIME FOR THE TIME STEP              717:        0.18187E+03

===============================================================


 INSTANT    0.718000000E+02   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         0.363128294E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160414E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
----------------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0093105                            30
a  epsilon                 -81.748                            56
a  Local Time Step      1.3764e-08                        281781


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7006          13.967          1.6255         0.39437
v  Velocity[Y]             -10.999          15.911           1.382         0.93892
v  Velocity[Z]              -16.68          10.554         -1.0386       -0.016071
v  ǁVelocityǁ            0.0094464          19.227          6.2422          7.4413
v  Pressure                 -27066      2.0144e+05      1.3233e+05      1.0623e+05
v  k                    5.5463e-07          4.8594        0.069317         0.11105
v  epsilon              0.00084544      1.1504e+06          1616.4          57.799
v  TurbVisc             1.8005e-12          0.5151       0.0035716         0.05034
v  CourantNb              0.093566      7.2652e+05          389.36          81.582
v  FourierNb               0.22706      2.3653e+06          219.01          3.4626
v  total_pressure       4.7293e+05      7.0144e+05      6.3233e+05      6.0623e+05
v  Local Time Step           -----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0093105                            30
a  epsilon                 -81.748                            56
a  Local Time Step      1.3764e-08                        281781


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7006          13.967          1.6255         0.39437
v  Velocity[Y]             -10.999          15.911           1.382         0.93892
v  Velocity[Z]              -16.68          10.554         -1.0386       -0.016071
v  ǁVelocityǁ            0.0094464          19.227          6.2422          7.4413
v  Pressure                 -27066      2.0144e+05      1.3233e+05      1.0623e+05
v  k                    5.5463e-07          4.8594        0.069317         0.11105
v  epsilon              0.00084544      1.1504e+06          1616.4          57.799
v  TurbVisc             1.8005e-12          0.5151       0.0035716         0.05034
v  CourantNb              0.093566      7.2652e+05          389.36          81.582
v  FourierNb               0.22706      2.3653e+06          219.01          3.4626
v  total_pressure       4.7293e+05      7.0144e+05      6.3233e+05      6.0623e+05
v  Local Time Step            0.01        0.047249            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7145      2.8423e+06          608.38          85.044


 TIME FOR THE TIME STEP              718:        0.18473E+03

===============================================================


 INSTANT    0.719000000E+02   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         0.181437784E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160431E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefi------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17286E+02 0.55410E+01
   Friction velocity        uet   :  0.41094E-01 0.35119E+02
   Friction velocity        uk    :  0.46717E-01 0.35119E+02
   Dimensionless distance   yplus :  0.40353E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13411
   Nb of faces within the viscous sub-layer     :      11360
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48744E+01     654   0.23620E+00   0.12705E+02 0.46459E+01 
c  Velocity[X]                                      0.35486E+01 
c  Velocity[Y]                                      0.68089E+01 
c  Velocity[Z]                                      0.23473E+01 
c  Pressure     0.11118E+00     580   0.90418E-02   0.23425E-01 0.75278E-01 
c  k            0.57897E+00     165   0.61497E-04   0.96710E-03 0.14059E+01 
c  epsilon      0.36009E+04      96   0.10946E-02   0.21282E+07 0.21689E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.010602                            39
a  epsilon                 -229.99                            61
a  Local Time Step       1.263e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7248          14.047          1.6716         0.39247
v  Velocity[Y]             -11.145          15.603          1.3356         0.93852
v  Velocity[Z]             -19.165          10.518         -1.0007       -0.016518
v  ǁVelocityǁ             0.028016          21.708          6.1784          7.4409
v  Pressure                 -27220      2.0172e+05       1.324e+05      1.0623e+05
v  k                    8.0085e-08          5.7278        0.069658         0.11114
v  epsilon              0.00018381      1.3925e+06            1684           58.02
v  TurbVisc             1.3009e-12          0.5151       0.0035822         0.05034
v  CourantNb               0.23037      7.9174e+05          395.94          81.548
v  FourierNb               0.22673      2.3653e+06          219.05          3.4639
v  total_pressure       4.7278e+05      7.0172e+05       6.324e+05      6.0623e+05
v  Local Time Step            0.01        0.057172            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               mi------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17286E+02 0.55410E+01
   Friction velocity        uet   :  0.41094E-01 0.35119E+02
   Friction velocity        uk    :  0.46717E-01 0.35119E+02
   Dimensionless distance   yplus :  0.40353E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13411
   Nb of faces within the viscous sub-layer     :      11360
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48744E+01     654   0.23620E+00   0.12705E+02 0.46459E+01 
c  Velocity[X]                                      0.35486E+01 
c  Velocity[Y]                                      0.68089E+01 
c  Velocity[Z]                                      0.23473E+01 
c  Pressure     0.11118E+00     580   0.90418E-02   0.23425E-01 0.75278E-01 
c  k            0.57897E+00     165   0.61497E-04   0.96710E-03 0.14059E+01 
c  epsilon      0.36009E+04      96   0.10946E-02   0.21282E+07 0.21689E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     ----------------------------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17286E+02 0.55410E+01
   Friction velocity        uet   :  0.41094E-01 0.35119E+02
   Friction velocity        uk    :  0.46717E-01 0.35119E+02
   Dimensionless distance   yplus :  0.40353E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13411
   Nb of faces within the viscous sub-layer     :      11360
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48744E+01     654   0.23620E+00   0.12705E+02 0.46459E+01 
c  Velocity[X]                                      0.35486E+01 
c  Velocity[Y]                                      0.68089E+01 
c  Velocity[Z]                                      0.23473E+01 
c  Pressure     0.11118E+00     580   0.90418E-02   0.23425E-01 0.75278E-01 
c  k            0.57897E+00     165   0.61497E-04   0.96710E-03 0.14059E+01 
c  epsilon      0.36009E+04      96   0.10946E-02   0.21282E+07 0.21689E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.010602                            39
a  epsilon                 -229.99                            61
a  Local Time Step       1.263e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7248          14.047          1.6716         0.39247
v  Velocity[Y]             -11.145          15.603          1.3356         0.93852
v  Velocity[Z]             -19.165          10.518         -1.0007       -0.016518
v  ǁVelocityǁ             0.028016          21.708          6.1784          7.4409
v  Pressure                 -27220      2.0172e+05       1.324e+05      1.0623e+05
v  k                    8.0085e-08          5.7278        0.069658         0.11114
v  epsilon              0.00018381      1.3925e+06            1684           58.02
v  TurbVisc             1.3009e-12          0.5151       0.0035822         0.05034
v  CourantNb               0.23037      7.9174e+05          395.94          81.548
v  FourierNb               0.22673      2.3653e+06          219.05          3.4639
v  total_pressure 
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5578      2.9196e+06          608.12          85.069


 TIME FOR THE TIME STEP              721:        0.17143E+03

===============================================================


 INSTANT    0.722000000E+02   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         0.260564061E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160418E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17027E+02 0.55411E+01
   Friction velocity        uet   :  0.38761E-01 0.36311E+02
   Friction velocity        uk    :  0.47397E-01 0.36311E+02
   Dimensionless distance   yplus :  0.42129E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13450
   Nb of faces within the viscous sub-layer     :      11413
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48798E+01     650   0.23452E+00   0.13784E+02 0.48362E+01 
c  Velocity[X]                                      0.35272E+01 
c  Velocity[Y]                                      0.83302E+01 
c  Velocity[Z]                                      0.19265E+01 
c  Pressure     0.10732E+00     851   0.84952E-02   0.22542E-01 0.59029E-01 
c  k            0.57894E+00     167   0.83442E-04   0.11856E-02 0.15565E+01 
c  epsilon      0.34416E+04     101   0.71934E-03   0.14134E+07 0.18499E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k        
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5578      2.9196e+06          608.12          85.069


 TIME FOR THE TIME STEP              721:        0.17146E+03

===============================================================


 INSTANT    0.722000000E+02   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         0.260564061E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160418E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
----------------------------------------------------------
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5578      2.9196e+06          608.12          85.069


 TIME FOR THE TIME STEP              721:        0.17907E+03

===============================================================


 INSTANT    0.722000000E+02   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         0.260564061E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160418E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17027E+02 0.55411E+01
   Friction velocity        uet   :  0.38761E-01 0.36311E+02
   Friction velocity        uk    :  0.47397E-01 0.36311E+02
   Dimensionless distance   yplus :  0.42129E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13450
   Nb of faces within the viscous sub-layer     :      11413
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48798E+01     650   0.23452E+00   0.13784E+02 0.48362E+01 
c  Velocity[X]                                      0.35272E+01 
c  Velocity[Y]                                      0.83302E+01 
c  Velocity[Z]                                      0.19265E+01 
c  Pressure     0.10732E+00     851   0.84952E-02   0.22542E-01 0.59029E-01 
c  k            0.57894E+00     167   0.83442E-04   0.11856E-02 0.15565E+01 
c  epsilon      0.34416E+04     101   0.71934E-03   0.14134E+07 0.18499E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0073851                            13
a  epsilon                 -484.19                            31
a  Local Time Step      1.3796e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7605          13.897           1.621         0.39264
v  Velocity[Y]             -11.132          15.966          1.3766         0.93706
v  Velocity[Z]             -17.332          10.735         -1.0415        -0.01594
v  ǁVelocityǁ            0.0055453          20.054          6.2548           7.446
v  Pressure                 -27353      2.0195e+05       1.325e+05      1.0628e+05
v  k                    3.1124e-07          5.3507         0.06923         0.11115
v  epsilon              0.00027371      1.2581e+06          1612.1          57.917
v  TurbVisc             1.8422e-12          0.5151       0.0035662        0.050343
v  CourantNb               0.26052      7.2483e+05          389.91          81.679
v  FourierNb               0.22668      2.3653e+06          219.01          3.4641
v  total_pressure       4.7265e+05      7.0195e+05       6.325e+05      6.0628e+05
v  Local Time Step            0.01        0.069178            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6476      2.7943e+06          608.92          85.143


 TIME FOR THE TIME STEP              722:        0.17725E+03

===============================================================


 INSTANT    0.723000000E+02   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         0.168861424E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160444E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
---------------------------------------------a  k                   -4.2295e-05                             3
a  epsilon                 -1.9799                             5
a  Local Time Step      1.3187e-08                        281781


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4791          14.064          1.6293         0.39177
v  Velocity[Y]             -11.092          15.972          1.3859          0.9363
v  Velocity[Z]              -17.35          10.164         -1.0595       -0.016156
v  ǁVelocityǁ            0.0069456          19.925           6.274          7.4436
v  Pressure                 -27442      2.0216e+05      1.3261e+05      1.0635e+05
v  k                    5.5591e-08          5.2713        0.070431         0.11122
v  epsilon               0.0071722      1.2472e+06          1682.7           58.37
v  TurbVisc             8.6595e-13          0.5151       0.0035677        0.050342
v  CourantNb               0.31263      7.5831e+05          396.35          81.758
v  FourierNb               0.22668      2.3653e+06          219.01          3.4627
v  total_pressure       4.7256e+05      7.0216e+05      6.3261e+05      6.0635e+05
v  Local Time Step            0.01        0.076096            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6a  k                   -4.2295e-05                             3
a  epsilon                 -1.9799                             5
a  Local Time Step      1.3187e-08                        281781


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4791          14.064          1.6293         0.39177
v  Velocity[Y]             -11.092          15.972          1.3859          0.9363
v  Velocity[Z]              -17.35          10.164         -1.0595       -0.016156
v  ǁVelocityǁ            0.0069456          19.925           6.274          7.4436
v  Pressure                 -27442      2.0216e+05      1.3261e+05      1.0635e+05
v  k                    5.5591e-08          5.2713        0.070431         0.11122
v  epsilon               0.0071722      1.2472e+06          1682.7           58.37
v  TurbVisc             8.6595e-13          0.5151       0.0035677        0.050342
v  CourantNb               0.31263      7.5831e+05          396.35          81.758
v  FourierNb               0.22668      2.3653e+06          219.01          3.4627
v  total_pressure       4.7256e+05      7.0216e+05      6.3261e+05      6.0635e+05
v  Local Time Step            0.01        0.076096            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6387      2.6475e+06          615.36          85.221


 TIME FOR THE TIME STEP              723:        0.18636E+03

===============================================================


 INSTANT    0.724000000E+02   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         0.279572333E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160424E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
----------------------------------   Dimensionless distance   yplus :  0.49275E-02 0.24879E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13415
   Nb of faces within the viscous sub-layer     :      11354
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48869E+01     648   0.24029E+00   0.10498E+02 0.42220E+01 
c  Velocity[X]                                      0.32571E+01 
c  Velocity[Y]                                      0.45775E+01 
c  Velocity[Z]                                      0.26631E+01 
c  Pressure     0.10189E+00     583   0.80057E-02   0.21293E-01 0.37604E-01 
c  k            0.57899E+00     170   0.64164E-04   0.10074E-02 0.14348E+01 
c  epsilon      0.34972E+04     100   0.78750E-03   0.14568E+07 0.18743E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0028249                            18
a  epsilon                 -166.93                            25
a  Local Time Step      1.1862e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3891           13.96          1.6481         0.39309
v  Velocity[Y]             -11.048          16.457          1.3342         0.93914
v  Velocity[Z]             -19.227          10.347         -1.0322       -0.015731
v  ǁVelocityǁ            0.0048409          21.779          6.2235           7.446
v  Pressure                 -27600      2.0233e+05      1.3268e+05      1.0641e+05
v  k                    4.8449e-07          5.2699        0.069076         0.11119
v  epsilon               0.0016583      1.2393e+06          1618.5          57.975
v  TurbVisc             1.6795e-12          0.5151       0.0035739        0.050346
v  CourantNb              0.015871      8.4305e+05           391.8          81.654
v  FourierNb               0.22696      2.3653e+06          219.04           3.464
v  total_pressure        4.724e+05      7.0233e+05      6.3268e+05      6.0641e+05
v  Local Time Step            0.01        0.092076        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6159      2.9687e+06          610.84          85.118


 TIME FOR THE TIME STEP              725:        0.16835E+03

===============================================================


 INSTANT    0.72   Dimensionless distance   yplus :  0.49275E-02 0.24879E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13415
   Nb of faces within the viscous sub-layer     :      11354
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48869E+01     648   0.24029E+00   0.10498E+02 0.42220E+01 
c  Velocity[X]                                      0.32571E+01 
c  Velocity[Y]                                      0.45775E+01 
c  Velocity[Z]                                      0.26631E+01 
c  Pressure     0.10189E+00     583   0.80057E-02   0.21293E-01 0.37604E-01 
c  k            0.57899E+00     170   0.64164E-04   0.10074E-02 0.14348E+01 
c  epsilon      0.34972E+04     100   0.78750E-03   0.14568E+07 0.18743E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0028249                            18
a  epsilon                 -166.93                            25
a  Local Time Step      1.1862e-08                        281782


     Dimensionless distance   yplus :  0.49275E-02 0.24879E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13415
   Nb of faces within the viscous sub-layer     :      11354
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48869E+01     648   0.24029E+00   0.10498E+02 0.42220E+01 
c  Velocity[X]                                      0.32571E+01 
c  Velocity[Y]                                      0.45775E+01 
c  Velocity[Z]                                      0.26631E+01 
c  Pressure     0.10189E+00     583   0.80057E-02   0.21293E-01 0.37604E-01 
c  k            0.57899E+00     170   0.64164E-04   0.10074E-02 0.14348E+01 
c  epsilon      0.34972E+04     100   0.78750E-03   0.14568E+07 0.18743E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0028249                            18
a  epsilon                 -166.93                            25
a  Local Time Step      1.1862e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3891           13.96          1.6481         0.39309
v  Velocity[Y]             -11.048          16.457          1.3342         0.93914
v  Velocity[Z]             -19.227          10.347         -1.0322       -0.015731
v  ǁVelocityǁ            0.0048409          21.779          6.2235           7.446
v  Pressure                 -27600      2.0233e+05      1.3268e+05      1.0641e+05
v  k                    4.8449e-07          5.2699        0.069076         0.11119
v  epsilon               0.0016583      1.2393e+06          1618.5          57.975
v  TurbVisc             1.6795e-12          0.5151       0.0035739        0.050346
v  CourantNb              0.015871      8.4305e+05           391.8          81.654
v  FourierNb               0.22696      2.3653e+06          219.04           3.464
v  total_pressure        4.724e+05      7.0233e+05      6.3268e+05      6.0641e+05
v  Local Time Step            0.01        0.092076        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
    INSTANT    0.727000000E+02   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         0.128372867E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160833E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17050E+02 0.55411E+01
   Friction velocity        uet   :  0.39961E-01 0.48596E+02
   Friction velocity        uk    :  0.45072E-01 0.48596E+02
   Dimensionless distance   yplus :  0.24135E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13495
   Nb of faces within the viscous sub-layer     :      11202
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48826E+01     668   0.24487E+00   0.11178E+02 0.43550E+01 
c  Velocity[X]                                      0.32948E+01 
c  Velocity[Y]                                      0.48739E+01 
c  Velocity[Z]                                      0.30097E+01 
c  Pressure     0.11068E+00    1070   0.85187E-02   0.23067E-01 0.12027E+00 
c  k            0.57905E+00     166   0.81847E-04   0.12357E-02 0.15889E+01 
c  epsilon      0.35734E+04     107   0.93975E-03   0.14485E+07 0.17902E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00097165                             9
a  epsilon                 -26.948                            20
a  Local Time Step      1.2795e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  INSTANT    0.727000000E+02   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         0.128372867E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160833E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17050E+02 0.55411E+01
   Friction velocity        uet   :  0.39961E-01 0.48596E+02
   Friction velocity        uk    :  0.45072E-01 0.48596E+02
   Dimensionless distance   yplus :  0.24135E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13495
   Nb of faces INSTANT    0.727000000E+02   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         0.128372867E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160833E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17050E+02 0.55411E+01
   Friction velocity        uet   :  0.39961E-01 0.48596E+02
   Friction velocity        uk    :  0.45072E-01 0.48596E+02
   Dimensionless distance   yplus :  0.24135E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13495
   Nb of faces within the viscous sub-layer     :      11202
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48826E+01     668   0.24487E+00   0.11178E+02 0.43550E+01 
c  Velocity[X]                                      0.32948E+01 
c  Velocity[Y]                                      0.48739E+01 
c  Velocity[Z]                                      0.30097E+01 
c  Pressure     0.11068E+00    1070   0.85187E-02   0.23067E-01 0.12027E+00 
c  k            0.57905E+00     166   0.81847E-04   0.12357E-02 0.15889E+01 
c  epsilon      0.35734E+04     107   0.93975E-03   0.14485E+07 0.17902E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00097165                             9
a  epsilon                 -26.948                            20
a  Local Time Step      1.2795e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4794          14.126          1.6286         0.39219
v  Velocity[Y]             -11.089          16.061          1.3936         0.93764
v  Velocity[Z]             -16.638          10.702         -1.0643       -0.015734
v  ǁVelocityǁ              0.02172          19.307          6.2822          7.4467
v  Pressure                 -27756      2.0261e+05      1.3282e+05      1.0653e+05
v  k                     5.475e-07           5.323        0.071225         0.11123
v  epsilon               0.0024731      1.2672e+06          1742.1          58.664
v  TurbVisc             2.5716e-13          0.5151       0.0035665         0.05034
v  CourantNb               0.32331      7.8153e+05          398.37          81.817
v  FourierNb                0.2268      2.3653e+06          219.04          3.4638
v  total_pressure       4.7224e+05      7.0261e+05      6.3282e+05      6.0653e+05
v  Local Time Step            0.01        0.073257            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6276      2.6974e+06          617.41           85.28


 TIME FOR THE TIME STEP              727:        0.18415E+03

===============================================================


 INSTANT    0.728000000E+02   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         0.102076129E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160456E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16927E+02 0.55410E+01
   Friction velocity        uet   :  0.43324E-01 0.46762E+02
   Friction velocity        uk    :  0.46666E-01 0.46762E+02
   Dimensionless distance   yplus :  0.34982E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of th-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7609          14.128           1.648          0.3922
v  Velocity[Y]             -10.969          16.017           1.349         0.93925
v  Velocity[Z]             -17.547          9.6741         -1.0343       -0.016199
v  ǁVelocityǁ             0.023064          20.227          6.1985          7.4458
v  Pressure                 -27772      2.0275e+05      1.3288e+05       1.066e+05
v  k                    2.7385e-07          5.6042        0.070848         0.11121
v  epsilon               0.0056965       1.361e+06          1751.1          58.448
v  TurbVisc              1.345e-12          0.5151       0.0035722        0.050342
v  CourantNb              0.010444      8.0804e+05          400.78          81.853
v  FourierNb               0.22675      2.3653e+06          219.05          3.4628
v  total_pressure       4.7223e+05      7.0275e+05      6.3288e+05       6.066e+05
v  Local Time Step            0.01        0.080583            0.01        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5958      2.9336e+06          619.84          85.316


 TIME FOR THE TIME STEP              728:        0.19066E+03

===============================================================


 INSTANT    0.729000000E+02   TIME STEP NUMBER             729
 ============================================================= 




   ** BOUNDARY MASS FLOW INF-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7609          14.128           1.648          0.3922
v  Velocity[Y]             -10.969          16.017           1.349         0.93925
v  Velocity[Z]             -17.547          9.6741         -1.0343       -0.016199
v  ǁVelocityǁ             0.023064          20.227          6.1985          7.4458
v  Pressure                 -27772      2.0275e+05      1.3288e+05       1.066e+05
v  k                    2.7385e-07          5.6042        0.070848         0.11121
v  epsilon               0.0056965       1.361e+06          1751.1          58.448
v  TurbVisc              1.345e-12          0.5151       0.0035722        0.050342
v  CourantNb              0.010444      8.0804e+05          400.78          81.853
v  FourierNb               0.22675      2.3653e+06          219.05          3.4628
v  total_pressure       4.7223e+05      7.0275e+05      6.3288e+05       6.066e+05
v  Local Time Step            0.01        0.080583            0.01        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5958      2.9336e+06          619.84          85.316


 TIME FOR THE TIME STEP              728:        0.16901E+03

===============================================================


 INSTANT    0.729000000E+02   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         0.133617586E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160423E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17088E+02 0.55410E+01
   Friction velocity        uet   :  0.36945E-01 0.49139E+02
   Friction velocity        uk    :  0.46123E-01 0.49139E+02
   Dimensionless distance   yplus :  0.32980E-02 0.24879E+02
   ----------------------------------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48834E+01     624   0.23383E+00   0.13455E+02 0.47743E+01 
c  Velocity[X]                                      0.32490E+01 
c  Velocity[Y]                                      0.78808E+01 
c  Velocity[Z]                                      0.23251E+01 
c  Pressure     0.10838E+00    1049   0.81312E-02   0.22524E-01 0.10007E+00 
c  k            0.57902E+00     166   0.62450E-04   0.10482E-02 0.14634E+01 
c  epsilon      0.35385E+04     108   0.45315E-03   0.47597E+06 0.10459E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00028542                             7
a  epsilon                 -9.3299                             6
a  Local Time Step      1.3363e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5947          14.044          1.6098         0.39399
v  Velocity[Y]             -11.381          15.798          1.3883         0.93837
v  Velocity[Z]             -19.293           10.92         -1.0684       -0.014196
v  ǁVelocityǁ            0.0033044          21.785          6.2869          7.4522
v  Pressure                 -27763      2.0302e+05      1.3305e+05      1.0676e+05
v  k                    7.6753e-08          5.4002         0.07068         0.11123
v  epsilon              9.9452e-05      1.2802e+06          1691.6          58.495
v  TurbVisc             1.7571e-12          0.5151       0.0035655        0.050341
v  CourantNb              0.090947      7.4835e+05          394.32          81.852
v  FourierNb               0.22647      2.3653e+06          219.03          3.4627
v  total_pressure       4.7224e+05      7.0302e+05      6.3305e+05      6.0676e+05
v  Local Time Step            0.01        0.097505        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier            1.48      2.6699e+06          613.34          85.315


 TIME FOR THE TIME STEP              730:        0.17864E+03

===============================================================


 INSTANT    0.731000000E+02   TIME STEP NUMBER             731
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces         ------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48834E+01     624   0.23383E+00   0.13455E+02 0.47743E+01 
c  Velocity[X]                                      0.32490E+01 
c  Velocity[Y]                                      0.78808E+01 
c  Velocity[Z]                                      0.23251E+01 
c  Pressure     0.10838E+00    1049   0.81312E-02   0.22524E-01 0.10007E+00 
c  k            0.57902E+00     166   0.62450E-04   0.10482E-02 0.14634E+01 
c  epsilon      0.35385E+04     108   0.45315E-03   0.47597E+06 0.10459E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00028542                             7
a  epsilon                 -9.3299                             6
a  Local Time Step      1.3363e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5947          14.044          1.6098         0.------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48834E+01     624   0.23383E+00   0.13455E+02 0.47743E+01 
c  Velocity[X]                                      0.32490E+01 
c  Velocity[Y]                                      0.78808E+01 
c  Velocity[Z]                                      0.23251E+01 
c  Pressure     0.10838E+00    1049   0.81312E-02   0.22524E-01 0.10007E+00 
c  k            0.57902E+00     166   0.62450E-04   0.10482E-02 0.14634E+01 
c  epsilon      0.35385E+04     108   0.45315E-03   0.47597E+06 0.10459E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00028542                             7
a  epsilon                 -9.3299                             6
a  Local Time Step      1.3363e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5947          14.044          1.6098         0.39399
v  Velocity[Y]             -11.381          15.798          1.3883         0.93837
v  Velocity[Z]             -19.293           10.92         -1.0684       -0.014196
v  ǁVelocityǁ            0.0033044          21.785          6.2869          7.4522
v  Pressure                 -27763      2.0302e+05      1.3305e+05      1.0676e+05
v  k                    7.6753e-08          5.4002         0.07068         0.11123
v  epsilon              9.9452e-05      1.2802e+06          1691.6          58.495
v  TurbVisc             1.7571e-12          0.5151       0.0035655        0.050341
v  CourantNb              0.090947      7.4835e+05          394.32          81.852
v  FourierNb               0.22647      2.3653e+06          219.03          3.4627
v  total_pressure       4.7224e+05      7.0302e+05      6.3305e+05      6.0676e+05
v  Local Time Step            0.01        0.097505        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier            1.48      2.6699e+06          613.34          85.315


 TIME FOR THE TIME STEP              730:        0.19052E+03

===============================================================


 INSTANT    0.731000000E+02   TIME STEP NUMBER             7Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.657256623E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160418E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17328E+02 0.55410E+01
   Friction velocity        uet   :  0.40751E-01 0.57427E+02
   Friction velocity        uk    :  0.44191E-01 0.57427E+02
   Dimensionless distance   yplus :  0.31970E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13444
   Nb of faces within the viscous sub-layer     :      11191
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48867E+01     651   0.24318E+00   0.14411E+02 0.49435E+01 
c  Velocity[X]                                      0.38224E+01 
c  Velocity[Y]                                      0.80524E+01 
c  Velocity[Z]                                      0.25367E+01 
c  Pressure     0.12243E+00    1017   0.89419E-02   0.25372E-01 0.73955E-01 
c  k            0.57901E+00     164   0.74697E-04   0.13841E-02 0.16818E+01 
c  epsilon      0.36967E+04     101   0.94786E-03   0.21952E+07 0.21434E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0011356                            27
a  epsilon                 -25.113                            61
a  Local Time Step      1.1387e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7331          14.176          1.6387         0.39339
v  Velocity[Y]             -11.115          15.948          1.3422         0.94002
v  Velocity[Z]             -16.843          11.386         -1.0491      Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.657256623E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160418E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17328E+02 0.55410E+01
   Friction velocity        uet   :  0.40751E-01 0.57427E+02
   Friction velocity        uk    :  0.44191E-01 0.57427E+02
   Dimensionless distance   yplus :  0.31970E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13444
   Nb of faces within the viscous sub-layer     :      11191
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
--------------------------------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.657256623E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160418E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17328E+02 0.55410E+01
   Friction velocity        uet   :  0.40751E-01 0.57427E+02
   Friction velocity        uk    :  0.44191E-01 0.57427E+02
   Dimensionless distance   yplus :  0.31970E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13444
   Nb of faces within the viscous sub-layer     :      11191
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48867E+01     651   0.24318E+00   0.14411E+02 0.49435E+01 
c  Velocity[X]                                      0.38224E+01 
c  Velocity[Y]                                      0.80524E+01 
c  Velocity[Z]                                      0.25367E+01 
c  Pressure     0.12243E+00    1017   0.89419E-02   0.25372E-01 0.73955E-01 
c  k            0.57901E+00     164   0.74697E-04   0.13841E-02 0.16818E+01 
c  epsilon      0.36967E+04     101   0.94786E-03   0.21952E+07 0.21434E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0011356                            27
a  epsilon                 -25.113                            61
a  Local Time Step      1.1387e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  ---v  Velocity[Z]             -16.037          10.264         -1.0495       -0.014621
v  ǁVelocityǁ             0.030727          19.254          6.2612          7.4509
v  Pressure                 -27567      2.0364e+05      1.3351e+05      1.0714e+05
v  k                    4.2026e-07          5.3292        0.069989         0.11112
v  epsilon              0.00035203      1.2658e+06          1676.8          58.239
v  TurbVisc             4.1364e-13          0.5151       0.0035808        0.050337
v  CourantNb               0.45998      7.2493e+05          394.38          81.699
v  FourierNb               0.22628      2.3653e+06          219.07          3.4633
v  total_pressure       4.7243e+05      7.0364e+05      6.3351e+05      6.0714e+05
v  Local Time Step            0.01        0.064081            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.637      2.8319e+06          613.45          85.162


 TIME FOR THE TIME STEP              733:        0.19586E+03

===============================================================


 INSTANT    0.734000000E+02   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         0.220048371E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160422E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17194E+02 0.55410E+01
   Friction velocity        uet   :  0.24725E-01 0.53978E+02
   Friction velocity        uk    :  0.24717E-01 0.53978E+02
   Dimensionless distance   yplus :  0.34828E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13495
   Nb of faces within the viscous sub-layer     :      11216
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-------------v  Velocity[Z]             -16.037          10.264         -1.0495       -0.014621
v  ǁVelocityǁ             0.030727          19.254          6.2612          7.4509
v  Pressure                 -27567      2.0364e+05      1.3351e+05      1.0714e+05
v  k                    4.2026e-07          5.3292        0.069989         0.11112
v  epsilon              0.00035203      1.2658e+06          1676.8          58.239
v  TurbVisc             4.1364e-13          0.5151       0.0035808        0.050337
v  CourantNb               0.45998      7.2493e+05          394.38          81.699
v  FourierNb               0.22628      2.3653e+06          219.07          3.4633
v  total_pressure       4.7243e+05      7.0364e+05      6.3351e+05      6.0714e+05
v  Local Time Step            0.01        0.064081            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.637      2.8319e+06          613.45          85.162


 TIME FOR THE TIME STEP              733:        0.18201E+03

===============================================================


 INSTANT    0.734000000E+02   TIME STEP NUMBER             734
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet         v  Velocity[Z]             -16.037          10.264         -1.0495       -0.014621
v  ǁVelocityǁ             0.030727          19.254          6.2612          7.4509
v  Pressure                 -27567      2.0364e+05      1.3351e+05      1.0714e+05
v  k                    4.2026e-07          5.3292        0.069989         0.11112
v  epsilon              0.00035203      1.2658e+06          1676.8          58.239
v  TurbVisc             4.1364e-13          0.5151       0.0035808        0.050337
v  CourantNb               0.45998      7.2493e+05          394.38          81.699
v  FourierNb               0.22628      2.3653e+06          219.07          3.4633
v  total_pressure       4.7243e+05      7.0364e+05      6.3351e+05      6.0714e+05
v  Local Time Step            0.01        0.064081            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.637      2.8319e+06          613.45          85.162


 TIME FOR THE TIME STEP              733:        0.19285E+03

===============================================================


 INSTANT    0.734000000E+02   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         0.220048371E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160422E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17194E+02 0.55410E+01
   Friction velocity        uet   :  0.24725E-01 0.53978E+02
   Friction velocity        uk    :  0.24717E-01 0.53978E+02
   Dimensionless distance   yplus :  0.34828E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13495
   Nb of faces within the viscous sub-layer     :      11216
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48854E+01     634   0.23308E+00   0.12599E+02 0.46184E+01 
c  Velocity[X]                                      0.32714E+01 
c  Velocity[Y]                                      0.70691E+01 
c  Velocity[Z]                                      0.22588E+01 
c  Pressure     0.11184E+00    1027   0.83331E-02   0.23158E-01 0.83120E-01 
c  k            0.57889E+00     164   0.62844E-04   0.10432E-02 0.14603E+01 
c  epsilon      0.35701E+04     110   0.65113E-03   0.58958E+06 0.11573E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.7417e-05                             5
a  epsilon                 -20.608                             5
a  Local Time Step      1.2856e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6121           14.11          1.6166         0.39491
v  Velocity[Y]             -11.027          16.014          1.3939         0.93968
v  Velocity[Z]             -18.824          11.162         -1.0838       -0.014137
v  ǁVelocityǁ             0.017743          21.466          6.2892          7.4547
v  Pressure                 -27556      2.0379e+05      1.3362e+05      1.0724e+05
v  k                    6.2805e-08          5.4345        0.070807         0.11109
v  epsilon               0.0058388      1.2933e+06          1698.6          58.412
v  TurbVisc             1.7476e-12          0.5151       0.0035684        0.050326
v  CourantNb               0.31814      7.7782e+05          395.89          81.917
v  FourierNb               0.22616      2.3653e+06          219.05          3.4629
v  total_pressure       4.7244e+05      7.0379e+05      6.3362e+05      6.0724e+05
v  Local Time Step            0.01        0.070489            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6267      2.6662e+06          614.94           85.38


 TIME FOR THE TIME STEP              734:        0.18724E+03

===============================================================


 INSTANT    0.735000000E+02   TIME STEP NUMBER             735
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
-----------------------------------------------------------------------------
c  Velocity     0.48991E+01     646   0.24517E+00   0.11686E+02 0.44496E+01 
c  Velocity[X]                                      0.33568E+01 
c  Velocity[Y]                                      0.55404E+01 
c  Velocity[Z]                                      0.27885E+01 
c  Pressure     0.11538E+00     940   0.85362E-02   0.23852E-01 0.43062E-01 
c  k            0.57892E+00     159   0.10634E-03   0.16247E-02 0.18223E+01 
c  epsilon      0.35970E+04     114   0.16351E-02   0.47594E+07 0.31267E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00031417                            26
a  epsilon                 -27.391                            22
a  Local Time Step      1.2378e-08                        281781


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6473          14.159          1.6361         0.39399
v  Velocity[Y]             -11.062          16.506          1.3932          0.9392
v  Velocity[Z]             -16.522          10.836          -1.073       -0.015008
v  ǁVelocityǁ            0.0095503          19.432          6.2985          7.4518
v  Pressure                 ------------------------------------------------------------------------------
c  Velocity     0.48991E+01     646   0.24517E+00   0.11686E+02 0.44496E+01 
c  Velocity[X]                                      0.33568E+01 
c  Velocity[Y]                                      0.55404E+01 
c  Velocity[Z]                                      0.27885E+01 
c  Pressure     0.11538E+00     940   0.85362E-02   0.23852E-01 0.43062E-01 
c  k            0.57892E+00     159   0.10634E-03   0.16247E-02 0.18223E+01 
c  epsilon      0.35970E+04     114   0.16351E-02   0.47594E+07 0.31267E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00031417                            26
a  epsilon                 -27.391                            22
a  Local Time Step      1.2378e-08                        281781


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6473          14.159          1.6361         0.39399
v  Velocity[Y]             -11.062          16.506          1.3932          0.9392
v  Velocity[Z]             -16.522          10.836          -1.073       -0.015008
v  ǁVelocityǁ            0.0095503          19.432          6.2985          7.4518
v  Pressure                 -27622       2.039e+05      1.3369e+05      1.0727e+05
v  k                     3.002e-07          5.2599        0.072302         0.11109
v  epsilon               0.0070657      1.2441e+06          1809.3          58.949
v  TurbVisc             6.3521e-14          0.5151       0.0035754         0.05032
v  CourantNb               0.24404      8.0785e+05          400.89          81.947
v  FourierNb               0.22593      2.3653e+06          219.07          3.4626
v  total_pressure       4.7238e+05       7.039e+05      6.3369e+05      6.0727e+05
v  Local Time Step            0.01        0.077538        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6394      2.8605e+06          619.96           85.41


 TIME FOR THE TIME STEP              735:        0.18319E+03

===============================================================


 INSTANT    0.736000000E+02   TIME STEP NUMBER             736
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
----------------------------------------------Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160433E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17266E+02 0.55410E+01
   Friction velocity        uet   :  0.31918E-01 0.34962E+02
   Friction velocity        uk    :  0.31582E-01 0.34962E+02
   Dimensionless distance   yplus :  0.22442E-02 0.24879E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13482
   Nb of faces within the viscous sub-layer     :      11177
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48858E+01     624   0.23954E+00   0.11227E+02 0.43619E+01 
c  Velocity[X]                                      0.37320E+01 
c  Velocity[Y]                                      0.49539E+01 
c  Velocity[Z]                                      0.25414E+01 
c  Pressure     0.11577E+00     671   0.81213E-02   0.23956E-01 0.28434E-01 
c  k            0.57900E+00     169   0.57336E-04   0.10289E-02 0.14500E+01 
c  epsilon      0.36251E+04     108   0.74610E-03   0.15237E+07 0.18281E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00051833                            35
a  epsilon                 -45.872                            50
a  Local Time Step      1.3746e-08                        281779


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5354          14.123          1.6264         0.39416
v  Velocity[Y]             -11.309          16.267           1.347         0.94061
v  Velocity[Z]              -16.52          10.704         -1.0499       -0.014928
v  ǁVelocityǁ              0.02055          19.237          6.2713          7.4534
v  Pressure                 -27697      2.0411e+05      1.3377e+05      1.0735e+05
v  k                    5.1554e-07          5.4525         0.07098         0.11118
v  epsilon               0.0029966      1.3106e+06    Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160433E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17266E+02 0.55410E+01
   Friction velocity        uet   :  0.31918E-01 0.34962E+02
   Friction velocity        uk    :  0.31582E-01 0.34962E+02
   Dimensionless distance   yplus :  0.22442E-02 0.24879E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13482
   Nb of faces within the viscous sub-layer     :      11177
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48858E+01     624   0.23954E+00   0.11227E+02 0.43619E+01 
c  Velocity[X]                       Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160433E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17266E+02 0.55410E+01
   Friction velocity        uet   :  0.31918E-01 0.34962E+02
   Friction velocity        uk    :  0.31582E-01 0.34962E+02
   Dimensionless distance   yplus :  0.22442E-02 0.24879E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13482
   Nb of faces within the viscous sub-layer     :      11177
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48858E+01     624   0.23954E+00   0.11227E+02 0.43619E+01 
c  Velocity[X]                                      0.37320E+01 
c  Velocity[Y]                                      0.49539E+01 
c  Velocity[Z]                                      0.25414E+01 
c  Pressure     0.11577E+00     671   0.81213E-02   0.23956E-01 0.28434E-01 
c  k            0.57900E+00     169   0.57336E-04   0.10289E-02 0.14500E+01 
c  epsilon      0.36251E+04     108   0.74610E-03   0.15237E+07 0.18281E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00051833                            35
a  epsilon                 -45.872                            50
a  Local Time Step      1.3746e-08                        281779


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5354          14.123          1.6264         0.39416
v  Velocity[Y]             -11.309          16.267           1.347         0.94061
v  Velocity[Z]              -16.52          10.704         -1.0499       -0.014928
v  ǁVelocityǁ              0.02055     v  epsilon               0.0025508      1.2853e+06          1698.4          58.559
v  TurbVisc             1.6363e-12          0.5151       0.0035733        0.050329
v  CourantNb              0.022121      7.9241e+05          397.17          81.946
v  FourierNb               0.22608      2.3653e+06          219.07           3.463
v  total_pressure       4.7225e+05      7.0416e+05      6.3377e+05      6.0736e+05
v  Local Time Step            0.01          0.1032        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6514      2.7328e+06          616.24          85.409


 TIME FOR THE TIME STEP              738:        0.17170E+03

===============================================================


 INSTANT    0.739000000E+02   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         0.104602791E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160444E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17048E+02 0.55410E+01
   Friction velocity        uet   :  0.24071E-01 0.43982E+02
   Friction velocity        uk    :  0.28743E-01 0.43982E+02
   Dimensionless distance   yplus :  0.30759E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13512
   Nb of faces within the viscous sub-layer     :      11109
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48929E+01     616   0.24316E+00   0.11798E+02 0.44676E+01 
c  Velocity[X]                                      0.31657E+01 
c  Velocity[Y]                                      0.61993E+01 
c  Velocity[Z]                                      0.24334E+0v  epsilon               0.0025508      1.2853e+06          1698.4          58.559
v  TurbVisc             1.6363e-12          0.5151       0.0035733        0.050329
v  CourantNb              0.022121      7.9241e+05          397.17          81.946
v  FourierNb               0.22608      2.3653e+06          219.07           3.463
v  total_pressure       4.7225e+05      7.0416e+05      6.3377e+05      6.0736e+05
v  Local Time Step            0.01          0.1032        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6514      2.7328e+06          616.24          85.409


 TIME FOR THE TIME STEP              738:        0.16468E+03

===============================================================


 INSTANT    0.739000000E+02   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         0.104602791E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160444E+01
Free inlet               13 v  epsilon               0.0025508      1.2853e+06          1698.4          58.559
v  TurbVisc             1.6363e-12          0.5151       0.0035733        0.050329
v  CourantNb              0.022121      7.9241e+05          397.17          81.946
v  FourierNb               0.22608      2.3653e+06          219.07           3.463
v  total_pressure       4.7225e+05      7.0416e+05      6.3377e+05      6.0736e+05
v  Local Time Step            0.01          0.1032        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6514      2.7328e+06          616.24          85.409


 TIME FOR THE TIME STEP              738:        0.17851E+03

===============================================================


 INSTANT    0.739000000E+02   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         0.104602791E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160444E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17048E+02 0.55410E+01
   Friction velocity        uet   :  0.24071E-01 0.43982E+02
   Friction velocity        uk    :  0.28743E-01 0.43982E+02
   Dimensionless distance   yplus :  0.30759E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13512
   Nb of faces within the viscous sub-layer     :      11109
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48929E+01     616   0.24316E+00   0.11798E+02 0.44676E+01 
c  Velocity[X]                                      0.31657E+01 
c  Velocity[Y]                                      0.61993E+01 
c  Velocity[Z]                                      0.24334E+01 
c  Pressure     0.11339E+00     872   0.82438E-02   0.23409E-01 0.33859E-01 
c  k            0.57908E+00     174   0.93699E-04   0.13146E-02 0.16385E+01 
c  epsilon      0.35981E+04     103   0.15433E-02   0.37080E+07 0.27845E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00037473                            43
a  epsilon                 -22.712                            74
a  Local Time Step      1.2256e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.669           14.23          1.6322         0.39248
v  Velocity[Y]             -11.024          16.531          1.3922         0.93771
v  Velocity[Z]             -16.881          10.326          -1.079       -0.014863
v  ǁVelocityǁ             0.023408          19.626           6.311          7.4565
v  Pressure                 -27798      2.0423e+05      1.3381e+05      1.0739e+05
v  k                    5.6468e-09           5.314        0.072258         0.11132
v  epsilon              0.00068213      1.2615e+06          1810.7          59.033
v  TurbVisc             1.5932e-12          0.5151       0.0035797        0.050338
v  CourantNb              0.028602      8.1594e+05          400.13          81.939
v  FourierNb               0.22649      2.3653e+06          219.08           3.463
v  total_pressure        4.722e+05      7.0423e+05      6.3381e+05      6.0739e+05
v  Local Time Step            0.01         0.11352        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6819      2.9416e+06          619.21          85.402


 TIME FOR THE TIME STEP              739:        0.18349E+03

===============================================================


 INSTANT    0.740000000E+02   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         0.706639039E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3  c  Velocity[Z]                                      0.25109E+01 
c  Pressure     0.11668E+00    1016   0.86296E-02   0.24085E-01 0.87076E-01 
c  k            0.57910E+00     173   0.59391E-04   0.10020E-02 0.14307E+01 
c  epsilon      0.37257E+04     110   0.95102E-03   0.23386E+07 0.21830E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00064938                            12
a  epsilon                 -21.399                            40
a  Local Time Step      1.1766e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7019          14.267          1.6143          0.3933
v  Velocity[Y]              -11.21          15.826          1.3503         0.93931
v  Velocity[Z]             -17.812          11.479         -1.0592       -0.015277
v  ǁVelocityǁ            0.0042352          20.544          6.2786          7.4529
v  Pressure                 -27780      2.0441e+05      1.3392e+05      1.0747e+05
v  k                    9.4072e-09          5.5623        0.071849         0.11131
v  epsilon              5.4454e-07      1.3531e+06          1815.8          58.793
v  TurbVisc             4.1848e-14          0.5151       0.003578c  Velocity[Z]                                      0.25109E+01 
c  Pressure     0.11668E+00    1016   0.86296E-02   0.24085E-01 0.87076E-01 
c  k            0.57910E+00     173   0.59391E-04   0.10020E-02 0.14307E+01 
c  epsilon      0.37257E+04     110   0.95102E-03   0.23386E+07 0.21830E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00064938                            12
a  epsilon                 -21.399                            40
a  Local Time Step      1.1766e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7019          14.267          1.6143          0.3933
v  Velocity[Y]              -11.21          15.826          1.3503         0.93931
v  Velocity[Z]             -17.812          11.479         -1.0592       -0.015277
v  ǁVelocityǁ            0.0042352          20.544          6.2786          7.4529
v  Pressure                 -27780      2.0441e+05      1.3392e+05      1.0747e+05
v  k                    9.4072e-09          5.5623        0.071849         0.11131
v  epsilon              5.4454e-07      1.3531e+06          1815.8          58.793
v  TurbVisc             4.1848e-14          0.5151       0.0035788        0.050346
v  CourantNb               0.29151      8.4991e+05          403.88          82.007
v  FourierNb               0.22684      2.3653e+06          219.09          3.4626
v  total_pressure       4.7222e+05      7.0441e+05      6.3392e+05      6.0747e+05
v  Local Time Step            0.01        0.062893            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5948      2.9755e+06          622.97           85.47


 TIME FOR THE TIME STEP              740:        0.17501E+03

===============================================================


 INSTANT    0.741000000E+02   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         0.365979306E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0       Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17031E+02 0.55409E+01
   Friction velocity        uet   :  0.43157E-01 0.35381E+02
   Friction velocity        uk    :  0.43105E-01 0.35381E+02
   Dimensionless distance   yplus :  0.33806E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13471
   Nb of faces within the viscous sub-layer     :      11171
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48876E+01     647   0.23407E+00   0.96971E+01 0.40518E+01 
c  Velocity[X]                                      0.26657E+01 
c  Velocity[Y]                                      0.46335E+01 
c  Velocity[Z]                                      0.23980E+01 
c  Pressure     0.11411E+00     834   0.83515E-02   0.23540E-01 0.28405E-01 
c  k            0.57Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17031E+02 0.55409E+01
   Friction velocity        uet   :  0.43157E-01 0.35381E+02
   Friction velocity        uk    :  0.43105E-01 0.35381E+02
   Dimensionless distance   yplus :  0.33806E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13471
   Nb of faces within the viscous sub-layer     :      11171
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48876E+01     647   0.23407E+00   0.96971E+01 0.40518E+01 
c  Velocity[X]                                      0.26657E+01 
c  Velocity[Y]                                      0.46335E+01 
c  Velocity[Z]                                      0.23980E+01 
c  Pressure     0.11411E+00     834   0.83515E-02   0.23540E-01 0.28405E-01 
c  k            0.578Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17031E+02 0.55409E+01
   Friction velocity        uet   :  0.43157E-01 0.35381E+02
   Friction velocity        uk    :  0.43105E-01 0.35381E+02
   Dimensionless distance   yplus :  0.33806E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13471
   Nb of faces within the viscous sub-layer     :      11171
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48876E+01     647   0.23407E+00   0.96971E+01 0.40518E+01 
c  Velocity[X]                                      0.26657E+01 
c  Velocity[Y]                                      0.46335E+01 
c  Velocity[Z]                                      0.23980E+01 
c  Pressure     0.11411E+00     834   0.83515E-02   0.23540E-01 0.28405E-01 
c  k            0.578Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17031E+02 0.55409E+01
   Friction velocity        uet   :  0.43157E-01 0.35381E+02
   Friction velocity        uk    :  0.43105E-01 0.35381E+02
   Dimensionless distance   yplus :  0.33806E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13471
   Nb of faces within the viscous sub-layer     :      11171
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48876E+01     647   0.23407E+00   0.96971E+01 0.40518E+01 
c  Velocity[X]                                      0.26657E+01 
c  Velocity[Y]                                      0.46335E+01 
c  Velocity[Z]                                      0.23980E+01 
c  Pressure     0.11411E+00     834   0.83515E-02   0.23540E-01 0.28405E-01 
c  k            0.57898E+00     165   0.77694E-04   0.11636E-02 0.15419E+01 
c  epsilon      0.35745E+04     115   0.95727E-03   0.24780E+07 0.23838E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.003633                            24
a  epsilon                 -318.85                            58
a  Local Time Step      1.2293e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6901          14.152           1.632         0.39421
v  Velocity[Y]             -11.061          15.889          1.3737         0.93892
v  Velocity[Z]               -19.4           11.18         -1.0761        -0.01411
v  ǁVelocityǁ             0.018838          22.042          6.2851          7.4551
v  Pressure                 -27850      2.0449e+05       1.339e+05      1.0747e+05
v  k                    5.8293e-07          5.4202        0.071069         0.11125
v  epsilon                0.006616     v  FourierNb               0.22652      2.3653e+06          219.09          3.4632
v  total_pressure       4.7203e+05      7.0448e+05      6.3386e+05      6.0742e+05
v  Local Time Step            0.01        0.083711        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6105       3.023e+06          618.89          85.429


 TIME FOR THE TIME STEP              743:        0.18058E+03

===============================================================


 INSTANT    0.744000000E+02   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         0.137720908E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160844E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17043E+02 0.55409E+01
   Friction velocity        uet   :  0.39922E-01 0.46411E+02
   Friction velocity        uk    :  0.39841E-01 0.46411E+02
   Dimensionless distance   yplus :  0.27390E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13510
   Nb of faces within the viscous sub-layer     :      11152
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48965E+01     637   0.24272E+00   0.11105E+02 0.43355E+01 
c  Velocity[X]                                      0.29492E+01 
c  Velocity[Y]                                      0.56459E+01 
c  Velocity[Z]                                      0.25103E+01 
c  Pressure     0.10978E+00     699   0.79588E-02   0.22638E-01 0.36000E-01 
c  k            0.57906E+00     164   0.68503E-04   0.96793E-03 0.14061E+01 
c  epsilon      0.36978E+04      98   0.13109E-02   0.26519E+07 0.23286E+02 
---------------v  FourierNb               0.22652      2.3653e+06          219.09          3.4632
v  total_pressure       4.7203e+05      7.0448e+05      6.3386e+05      6.0742e+05
v  Local Time Step            0.01        0.083711        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6105       3.023e+06          618.89          85.429


 TIME FOR THE TIME STEP              743:        0.18017E+03

===============================================================


 INSTANT    0.744000000E+02   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         0.137720908E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160844E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------v  FourierNb               0.22652      2.3653e+06          219.09          3.4632
v  total_pressure       4.7203e+05      7.0448e+05      6.3386e+05      6.0742e+05
v  Local Time Step            0.01        0.083711        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6105       3.023e+06          618.89          85.429


 TIME FOR THE TIME STEP              743:        0.17635E+03

===============================================================


 INSTANT    0.744000000E+02   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         0.137720908E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160844E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17043E+02 0.55409E+01
   Friction velocity        uet   :  0.39922E-01 0.46411E+02
   Friction velocity        uk    :  0.39841E-01 0.46411E+02
   Dimensionless distance   yplus :  0.27390E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13510
   Nb of faces within the viscous sub-layer     :      11152
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48965E+01     637   0.24272E+00   0.11105E+02 0.43355E+01 
c  Velocity[X]                                      0.29492E+01 
c  Velocity[Y]                                      0.56459E+01 
c  Velocity[Z]                                      0.25103E+01 
c  Pressure     0.10978E+00     699   0.79588E-02   0.22638E-01 0.36000E-01 
c  k            0.57906E+00     164   0.68503E-04   0.96793E-03 0.14061E+01 
c  epsilon      0.36978E+04      98   0.13109E-02   0.26519E+07 0.23286E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00033359                            10
a  epsilon                 -15.109                            16
a  Local Time Step      1.3121e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7162          14.181          1.6102         0.39377
v  Velocity[Y]             -11.108          15.828          1.3633         0.93942
v  Velocity[Z]             -17.386          10.321         -1.0556       -0.015278
v  ǁVelocityǁ             0.015109          20.088          6.3035           7.455
v  Pressure                 -28098      2.0457e+05      1.3388e+05      1.0742e+05
v  k                      5.54e-07           5.523         0.07195         0.11125
v  epsilon              0.00037585      1.3418e+06          1824.3          58.816
v  TurbVisc             1.8758e-12          0.5151       0.0035784         0.05033
v  CourantNb               0.11181      7.6215e+05             403          82.051
v  FourierNb               0.22628      2.3653e+06          219.09          3.4625
v  total_pressure        4.719e+05      7.0457e+05      6.3388e+05      6.0742e+05
v  Local Time Step            0.01        0.092082        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6318      2.8878e+06          622.08          85.513


 TIME FOR THE TIME STEP              744:        0.17902E+03

===============================================================


 INSTANT    0.745000000E+02   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        -0.138491556E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160463E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
----------------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00056787                             8
a  epsilon                 -7.3491                             7
a  Local Time Step      1.2864e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.462          14.192          1.6336         0.39374
v  Velocity[Y]             -11.255          15.939          1.3537         0.93965
v  Velocity[Z]              -17.71          11.344          -1.046       -0.015052
v  ǁVelocityǁ             0.014379          20.443          6.2663          7.4585
v  Pressure                 -28198      2.0457e+05      1.3382e+05      1.0737e+05
v  k                    5.0353e-07          5.9381        0.072052         0.11133
v  epsilon               0.0074927      1.3588e+06          1810.8          58.906
v  TurbVisc             1.6136e-12          0.5151       0.0035841        0.050335
v  CourantNb               0.17477      7.7737e+05          402.22          81.946
v  FourierNb               0.22619      2.3653e+06          219.09          3.4639
v  total_pressure        4.718e+05      7.0457e+05      6.3382e+05      6.0737e+05
v  Local Time Step           -----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00056787                             8
a  epsilon                 -7.3491                             7
a  Local Time Step      1.2864e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.462          14.192          1.6336         0.39374
v  Velocity[Y]             -11.255          15.939          1.3537         0.93965
v  Velocity[Z]              -17.71          11.344          -1.046       -0.015052
v  ǁVelocityǁ             0.014379          20.443          6.2663          7.4585
v  Pressure                 -28198      2.0457e+05      1.3382e+05      1.0737e+05
v  k                    5.0353e-07          5.9381        0.072052         0.11133
v  epsilon               0.0074927      1.3588e+06          1810.8          58.906
v  TurbVisc             1.6136e-12          0.5151       0.0035841        0.050335
v  CourantNb               0.17477      7.7737e+05          402.22          81.946
v  FourierNb               0.22619      2.3653e+06          219.09          3.4639
v  total_pressure        4.718e+05      7.0457e+05      6.3382e+05      6.0737e+05
v  Local Time Step            0.01         0.10129        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5792      2.7057e+06          621.31           85.41


 TIME FOR THE TIME STEP              745:        0.18462E+03

===============================================================


 INSTANT    0.746000000E+02   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         0.125147621E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160828E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefi------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17043E+02 0.55410E+01
   Friction velocity        uet   :  0.27985E-01 0.54486E+02
   Friction velocity        uk    :  0.27976E-01 0.54486E+02
   Dimensionless distance   yplus :  0.28097E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13499
   Nb of faces within the viscous sub-layer     :      11172
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48920E+01     623   0.23926E+00   0.12828E+02 0.46552E+01 
c  Velocity[X]                                      0.31344E+01 
c  Velocity[Y]                                      0.74620E+01 
c  Velocity[Z]                                      0.22320E+01 
c  Pressure     0.10643E+00     920   0.78330E-02   0.21899E-01 0.34044E-01 
c  k            0.57911E+00     171   0.59178E-04   0.85300E-03 0.13199E+01 
c  epsilon      0.35516E+04     102   0.58635E-03   0.77330E+06 0.13266E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0005692                            10
a  epsilon                 -3.4485                            15
a  Local Time Step      1.1353e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6262          14.194          1.6311         0.39379
v  Velocity[Y]             -11.123          16.369          1.3863         0.93883
v  Velocity[Z]             -15.571          9.5123         -1.0428       -0.014461
v  ǁVelocityǁ             0.012087          19.365          6.2935          7.4631
v  Pressure                 -28361      2.0454e+05      1.3373e+05      1.0731e+05
v  k                    1.2802e-07          5.2789        0.071007         0.11138
v  epsilon              0.00012741      1.2472e+06          1699.6          58.729
v  TurbVisc             1.6993e-12          0.5151       0.0035824        0.050351
v  CourantNb              0.074472      8.8084e+05          398.06          81.963
v  FourierNb               0.22681      2.3653e+06          219.06          3.4642
v  total_pressure       4.7164e+05      7.0454e+05      6.3373e+05      6.0731e+05
v  Local Time Step            0.01        0.049423            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               mi------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17043E+02 0.55410E+01
   Friction velocity        uet   :  0.27985E-01 0.54486E+02
   Friction velocity        uk    :  0.27976E-01 0.54486E+02
   Dimensionless distance   yplus :  0.28097E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13499
   Nb of faces within the viscous sub-layer     :      11172
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48920E+01     623   0.23926E+00   0.12828E+02 0.46552E+01 
c  Velocity[X]                                      0.31344E+01 
c  Velocity[Y]                                      0.74620E+01 
c  Velocity[Z]                                      0.22320E+01 
c  Pressure     0.10643E+00     920   0.78330E-02   0.21899E-01 0.34044E-01 
c  k            0.57911E+00     171   0.59178E-04   0.85300E-03 0.13199E+01 
c  epsilon      0.35516E+04     102   0.58635E-03   0.77330E+06 0.13266E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     ----------------------------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17043E+02 0.55410E+01
   Friction velocity        uet   :  0.27985E-01 0.54486E+02
   Friction velocity        uk    :  0.27976E-01 0.54486E+02
   Dimensionless distance   yplus :  0.28097E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13499
   Nb of faces within the viscous sub-layer     :      11172
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48920E+01     623   0.23926E+00   0.12828E+02 0.46552E+01 
c  Velocity[X]                                      0.31344E+01 
c  Velocity[Y]                                      0.74620E+01 
c  Velocity[Z]                                      0.22320E+01 
c  Pressure     0.10643E+00     920   0.78330E-02   0.21899E-01 0.34044E-01 
c  k            0.57911E+00     171   0.59178E-04   0.85300E-03 0.13199E+01 
c  epsilon      0.35516E+04     102   0.58635E-03   0.77330E+06 0.13266E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0005692                            10
a  epsilon                 -3.4485                            15
a  Local Time Step      1.1353e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6262          14.194          1.6311         0.39379
v  Velocity[Y]             -11.123          16.369          1.3863         0.93883
v  Velocity[Z]             -15.571          9.5123         -1.0428       -0.014461
v  ǁVelocityǁ             0.012087          19.365          6.2935          7.4631
v  Pressure                 -28361      2.0454e+05      1.3373e+05      1.0731e+05
v  k                    1.2802e-07          5.2789        0.071007         0.11138
v  epsilon              0.00012741      1.2472e+06          1699.6          58.729
v  TurbVisc             1.6993e-12          0.5151       0.0035824        0.050351
v  CourantNb              0.074472      8.8084e+05          398.06          81.963
v  FourierNb               0.22681      2.3653e+06          219.06          3.4642
v  total_pressure 
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5979      2.7913e+06          619.27           85.53


 TIME FOR THE TIME STEP              748:        0.18211E+03

===============================================================


 INSTANT    0.749000000E+02   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         0.280469293E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160431E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16899E+02 0.55410E+01
   Friction velocity        uet   :  0.33112E-01 0.45648E+02
   Friction velocity        uk    :  0.37291E-01 0.45648E+02
   Dimensionless distance   yplus :  0.32571E-02 0.24879E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13496
   Nb of faces within the viscous sub-layer     :      11157
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
------------------------------------------------------------------
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5979      2.7913e+06          619.27           85.53


 TIME FOR THE TIME STEP              748:        0.18379E+03

===============================================================


 INSTANT    0.749000000E+02   TIME STEP NUMBER             749
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smo
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5979      2.7913e+06          619.27           85.53


 TIME FOR THE TIME STEP              748:        0.17890E+03

===============================================================


 INSTANT    0.749000000E+02   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         0.280469293E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160431E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
----------------------------------------------------------
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5979      2.7913e+06          619.27           85.53


 TIME FOR THE TIME STEP              748:        0.17418E+03

===============================================================


 INSTANT    0.749000000E+02   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         0.280469293E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160431E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16899E+02 0.55410E+01
   Friction velocity        uet   :  0.33112E-01 0.45648E+02
   Friction velocity        uk    :  0.37291E-01 0.45648E+02
   Dimensionless distance   yplus :  0.32571E-02 0.24879E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13496
   Nb of faces within the viscous sub-layer     :      11157
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48947E+01     668   0.24018E+00   0.13123E+02 0.47112E+01 
c  Velocity[X]                                      0.34826E+01 
c  Velocity[Y]                                      0.74138E+01 
c  Velocity[Z]                                      0.22261E+01 
c  Pressure     0.10666E+00     906   0.76276E-02   0.21933E-01 0.31674E-01 
c  k            0.57913E+00     157   0.62001E-04   0.10264E-02 0.14477E+01 
c  epsilon      0.36906E+04     109   0.51072E-03   0.12819E+07 0.16413E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00029922                             6
a  epsilon                 -40.707                             9
a  Local Time Step      1.2425e-08                        281781


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3967          14.207          1.6361         0.39353
v  Velocity[Y]             -11.309          16.047          1.3512         0.94009
v  Velocity[Z]             -17.702          10.848         -1.0576       -0.014591
v  ǁVelocityǁ             0.020196          20.425          6.2684          7.4581
v  Pressure                 -28305      2.0476e+05      1.3387e+05      1.0739e+05
v  k                    5.5938e-07          5.5364        0.071768         0.11138
v  epsilon               0.0059106      1.3433e+06          1767.1          58.984
v  TurbVisc             4.0406e-13          0.5151       0.0035825        0.050356
v  CourantNb               0.23154      8.0484e+05          402.76          82.036
v  FourierNb               0.22722      2.3653e+06          219.06          3.4639
v  total_pressure        4.717e+05      7.0476e+05      6.3387e+05      6.0739e+05
v  Local Time Step            0.01        0.059802            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6998      2.7376e+06          621.82            85.5


 TIME FOR THE TIME STEP              749:        0.18326E+03

===============================================================


 INSTANT    0.750000000E+02   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         0.149964465E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160437E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
---------------------------------------------a  k                    -0.0019295                            49
a  epsilon                 -70.414                            96
a  Local Time Step      1.2378e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7316          14.137          1.6585          0.3936
v  Velocity[Y]             -11.221          16.086           1.352         0.94062
v  Velocity[Z]             -15.887          10.639         -1.0508       -0.014132
v  ǁVelocityǁ            0.0084986          19.236          6.2683          7.4574
v  Pressure                 -28287      2.0476e+05      1.3387e+05      1.0741e+05
v  k                    4.5881e-07          5.4667        0.070761         0.11134
v  epsilon               0.0020376      1.3074e+06          1692.3          58.663
v  TurbVisc             1.4764e-12          0.5151       0.0035972        0.050352
v  CourantNb              0.022228      8.0792e+05          398.15          81.987
v  FourierNb               0.22721      2.3653e+06          219.09          3.4644
v  total_pressure       4.7171e+05      7.0476e+05      6.3387e+05      6.0741e+05
v  Local Time Step            0.01        0.065782            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5a  k                    -0.0019295                            49
a  epsilon                 -70.414                            96
a  Local Time Step      1.2378e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7316          14.137          1.6585          0.3936
v  Velocity[Y]             -11.221          16.086           1.352         0.94062
v  Velocity[Z]             -15.887          10.639         -1.0508       -0.014132
v  ǁVelocityǁ            0.0084986          19.236          6.2683          7.4574
v  Pressure                 -28287      2.0476e+05      1.3387e+05      1.0741e+05
v  k                    4.5881e-07          5.4667        0.070761         0.11134
v  epsilon               0.0020376      1.3074e+06          1692.3          58.663
v  TurbVisc             1.4764e-12          0.5151       0.0035972        0.050352
v  CourantNb              0.022228      8.0792e+05          398.15          81.987
v  FourierNb               0.22721      2.3653e+06          219.09          3.4644
v  total_pressure       4.7171e+05      7.0476e+05      6.3387e+05      6.0741e+05
v  Local Time Step            0.01        0.065782            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5959      2.9246e+06          617.24          85.452


 TIME FOR THE TIME STEP              750:        0.16223E+03

===============================================================


 INSTANT    0.751000000E+02   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        -0.437803820E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160479E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
----------------------------------   Dimensionless distance   yplus :  0.30358E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13524
   Nb of faces within the viscous sub-layer     :      11186
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48978E+01     631   0.24446E+00   0.13904E+02 0.48494E+01 
c  Velocity[X]                                      0.43903E+01 
c  Velocity[Y]                                      0.67020E+01 
c  Velocity[Z]                                      0.28117E+01 
c  Pressure     0.11045E+00     460   0.78147E-02   0.22687E-01 0.36865E-01 
c  k            0.57914E+00     161   0.71716E-04   0.10271E-02 0.14482E+01 
c  epsilon      0.35730E+04     101   0.83570E-03   0.14673E+07 0.18013E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00091279                            10
a  epsilon                 -40.906                            28
a  Local Time Step      1.3029e-08                        281781


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7534          14.129          1.6135         0.39272
v  Velocity[Y]             -11.331          15.767          1.3868         0.93987
v  Velocity[Z]             -15.946          10.944         -1.0778       -0.014623
v  ǁVelocityǁ              0.01591          18.831          6.3489          7.4592
v  Pressure                 -28409      2.0482e+05      1.3385e+05      1.0737e+05
v  k                    5.3439e-07          5.4272        0.071573         0.11136
v  epsilon              0.00074889      1.3046e+06            1748          58.862
v  TurbVisc             1.8056e-   Dimensionless distance   yplus :  0.30358E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13524
   Nb of faces within the viscous sub-layer     :      11186
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48978E+01     631   0.24446E+00   0.13904E+02 0.48494E+01 
c  Velocity[X]                                      0.43903E+01 
c  Velocity[Y]                      Dimensionless distance   yplus :  0.30358E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13524
   Nb of faces within the viscous sub-layer     :      11186
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48978E+01     631   0.24446E+00   0.13904E+02 0.48494E+01 
c  Velocity[X]                                      0.43903E+01 
c  Velocity[Y]                                      0.67020E+01 
c  Velocity[Z]                                      0.28117E+01 
c  Pressure     0.11045E+00     460   0.78147E-02   0.22687E-01 0.36865E-01 
c  k            0.57914E+00     161   0.71716E-04   0.10271E-02 0.14482E+01 
c  epsilon      0.35730E+04     101   0.83570E-03   0.14673E+07 0.18013E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00091279                            10
a  epsilon                 -40.906                            28
a  Local Time Step      1.3029e-08                        281781


     Dimensionless distance   yplus :  0.30358E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13524
   Nb of faces within the viscous sub-layer     :      11186
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48978E+01     631   0.24446E+00   0.13904E+02 0.48494E+01 
c  Velocity[X]                                      0.43903E+01 
c  Velocity[Y]                                      0.67020E+01 
c  Velocity[Z]                                      0.28117E+01 
c  Pressure     0.11045E+00     460   0.78147E-02   0.22687E-01 0.36865E-01 
c  k            0.57914E+00     161   0.71716E-04   0.10271E-02 0.14482E+01 
c  epsilon      0.35730E+04     101   0.83570E-03   0.14673E+07 0.18013E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00091279                            10
a  epsilon                 -40.906                            28
a  Local Time Step      1.3029e-08                        281781


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7534          14.129          1.6135         0.39272
v  Velocity[Y]             -11.331          15.767          1.3868         0.93987
v  Velocity[Z]             -15.946          10.944         -1.0778       -0.014623
v  ǁVelocityǁ              0.01591          18.831          6.3489          7.4592
v  Pressure                 -28409      2.0482e+05      1.3385e+05      1.0737e+05
v  k                    5.3439e-07          5.4272        0.071573         0.11136
v  epsilon              0.00074889      1.3046e+06            1748          58.862
v  TurbVisc             1.8056e-12          0.5151       0.0035746        0.050345
v  CourantNb             0.0073721       7.675e+05          399.33          82.075
v  FourierNb               0.22696      2.3653e+06          219.05          3.4618
v  total_pressure       4.7159e+05      7.0482e+05      6.3385e+05      6.0737e+05
v  Local Time Step            0.01        0.079597            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
    INSTANT    0.754000000E+02   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        -0.167721452E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160433E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16877E+02 0.55409E+01
   Friction velocity        uet   :  0.43600E-01 0.59712E+02
   Friction velocity        uk    :  0.47462E-01 0.59712E+02
   Dimensionless distance   yplus :  0.25026E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13504
   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     0.48988E+01     629   0.24643E+00   0.13192E+02 0.47258E+01 
c  Velocity[X]                                      0.42514E+01 
c  Velocity[Y]                                      0.58994E+01 
c  Velocity[Z]                                      0.30408E+01 
c  Pressure     0.11577E+00     901   0.82147E-02   0.23772E-01 0.34861E-01 
c  k            0.57916E+00     177   0.61296E-04   0.10502E-02 0.14646E+01 
c  epsilon      0.36212E+04     104   0.74263E-03   0.15716E+07 0.18718E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0045324                            37
a  epsilon                  -128.3                            63
a  Local Time Step      1.0835e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  INSTANT    0.754000000E+02   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        -0.167721452E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160433E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16877E+02 0.55409E+01
   Friction velocity        uet   :  0.43600E-01 0.59712E+02
   Friction velocity        uk    :  0.47462E-01 0.59712E+02
   Dimensionless distance   yplus :  0.25026E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13504
   Nb of faces INSTANT    0.754000000E+02   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        -0.167721452E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160433E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16877E+02 0.55409E+01
   Friction velocity        uet   :  0.43600E-01 0.59712E+02
   Friction velocity        uk    :  0.47462E-01 0.59712E+02
   Dimensionless distance   yplus :  0.25026E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13504
   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     0.48988E+01     629   0.24643E+00   0.13192E+02 0.47258E+01 
c  Velocity[X]                                      0.42514E+01 
c  Velocity[Y]                                      0.58994E+01 
c  Velocity[Z]                                      0.30408E+01 
c  Pressure     0.11577E+00     901   0.82147E-02   0.23772E-01 0.34861E-01 
c  k            0.57916E+00     177   0.61296E-04   0.10502E-02 0.14646E+01 
c  epsilon      0.36212E+04     104   0.74263E-03   0.15716E+07 0.18718E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0045324                            37
a  epsilon                  -128.3                            63
a  Local Time Step      1.0835e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5337          14.112          1.6566         0.39305
v  Velocity[Y]             -11.117          16.219          1.3307          0.9416
v  Velocity[Z]             -14.697           10.48         -1.0222       -0.014741
v  ǁVelocityǁ              0.01726           19.38           6.253          7.4572
v  Pressure                 -28393      2.0487e+05      1.3385e+05      1.0739e+05
v  k                       2.4e-07          5.5035        0.070735         0.11141
v  epsilon               0.0053387      1.3207e+06          1704.7          58.709
v  TurbVisc             1.5639e-12          0.5151       0.0035927        0.050353
v  CourantNb               0.30423       9.229e+05          400.05          81.952
v  FourierNb               0.22715      2.3653e+06          219.09          3.4639
v  total_pressure       4.7161e+05      7.0487e+05      6.3385e+05      6.0739e+05
v  Local Time Step            0.01        0.096312            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6052      3.0485e+06          619.14          85.416


 TIME FOR THE TIME STEP              754:        0.18366E+03

===============================================================


 INSTANT    0.755000000E+02   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         0.137092042E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160833E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16788E+02 0.55409E+01
   Friction velocity        uet   :  0.35771E-01 0.46691E+02
   Friction velocity        uk    :  0.35416E-01 0.46691E+02
   Dimensionless distance   yplus :  0.25393E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of th-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6492          14.103           1.618         0.39406
v  Velocity[Y]             -11.346          15.842          1.3444         0.94048
v  Velocity[Z]             -18.556          9.7859         -1.0396        -0.01441
v  ǁVelocityǁ              0.02222          21.256          6.2846            7.46
v  Pressure                 -28402      2.0484e+05      1.3379e+05      1.0734e+05
v  k                    7.2005e-08          5.2755        0.069847         0.11137
v  epsilon                 0.00153      1.2364e+06          1627.3          58.478
v  TurbVisc             1.8553e-12          0.5151       0.0035778        0.050356
v  CourantNb               0.26116      7.9307e+05          394.83          81.982
v  FourierNb               0.22725      2.3653e+06          219.06          3.4643
v  total_pressure        4.716e+05      7.0484e+05      6.3379e+05      6.0734e+05
v  Local Time Step            0.01        0.048974            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5927      2.9187e+06          613.89          85.446


 TIME FOR THE TIME STEP              755:        0.17474E+03

===============================================================


 INSTANT    0.756000000E+02   TIME STEP NUMBER             756
 ============================================================= 




   ** BOUNDARY MASS FLOW INF-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6492          14.103           1.618         0.39406
v  Velocity[Y]             -11.346          15.842          1.3444         0.94048
v  Velocity[Z]             -18.556          9.7859         -1.0396        -0.01441
v  ǁVelocityǁ              0.02222          21.256          6.2846            7.46
v  Pressure                 -28402      2.0484e+05      1.3379e+05      1.0734e+05
v  k                    7.2005e-08          5.2755        0.069847         0.11137
v  epsilon                 0.00153      1.2364e+06          1627.3          58.478
v  TurbVisc             1.8553e-12          0.5151       0.0035778        0.050356
v  CourantNb               0.26116      7.9307e+05          394.83          81.982
v  FourierNb               0.22725      2.3653e+06          219.06          3.4643
v  total_pressure        4.716e+05      7.0484e+05      6.3379e+05      6.0734e+05
v  Local Time Step            0.01        0.048974            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5927      2.9187e+06          613.89          85.446


 TIME FOR THE TIME STEP              755:        0.19243E+03

===============================================================


 INSTANT    0.756000000E+02   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         0.111756147E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160830E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17108E+02 0.55409E+01
   Friction velocity        uet   :  0.28723E-01 0.58405E+02
   Friction velocity        uk    :  0.49045E-01 0.58405E+02
   Dimensionless distance   yplus :  0.34633E-02 0.24880E+02
   ----------------------------------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48985E+01     673   0.24447E+00   0.13873E+02 0.48433E+01 
c  Velocity[X]                                      0.33334E+01 
c  Velocity[Y]                                      0.76961E+01 
c  Velocity[Z]                                      0.28439E+01 
c  Pressure     0.11418E+00    1053   0.81345E-02   0.23419E-01 0.10850E+00 
c  k            0.57904E+00     170   0.94993E-04   0.13547E-02 0.16637E+01 
c  epsilon      0.36791E+04     101   0.10014E-02   0.28588E+07 0.24448E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0033964                            12
a  epsilon                 -281.03                            15
a  Local Time Step      1.1808e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.8284          14.159          1.6381         0.39314
v  Velocity[Y]              -11.21          16.423          1.3655         0.93899
v  Velocity[Z]             -15.781          11.122         -1.0562       -0.014891
v  ǁVelocityǁ             0.013203          19.331          6.2918           7.457
v  Pressure                 -28307      2.0505e+05      1.3395e+05      1.0744e+05
v  k                    4.9527e-07          5.4194        0.071962          0.1113
v  epsilon               0.0054008      1.3019e+06          1779.5           59.08
v  TurbVisc             1.6168e-12          0.5151       0.0035701        0.050347
v  CourantNb               0.48881      8.4689e+05          406.39          82.211
v  FourierNb               0.22705      2.3653e+06          219.07          3.4631
v  total_pressure       4.7169e+05      7.0505e+05      6.3395e+05      6.0744e+05
v  Local Time Step            0.01        0.057375            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6303      2.8216e+06          625.47          85.675


 TIME FOR THE TIME STEP              757:        0.18924E+03

===============================================================


 INSTANT    0.758000000E+02   TIME STEP NUMBER             758
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces         ------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48985E+01     673   0.24447E+00   0.13873E+02 0.48433E+01 
c  Velocity[X]                                      0.33334E+01 
c  Velocity[Y]                                      0.76961E+01 
c  Velocity[Z]                                      0.28439E+01 
c  Pressure     0.11418E+00    1053   0.81345E-02   0.23419E-01 0.10850E+00 
c  k            0.57904E+00     170   0.94993E-04   0.13547E-02 0.16637E+01 
c  epsilon      0.36791E+04     101   0.10014E-02   0.28588E+07 0.24448E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0033964                            12
a  epsilon                 -281.03                            15
a  Local Time Step      1.1808e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.8284          14.159          1.6381         0.------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48985E+01     673   0.24447E+00   0.13873E+02 0.48433E+01 
c  Velocity[X]                                      0.33334E+01 
c  Velocity[Y]                                      0.76961E+01 
c  Velocity[Z]                                      0.28439E+01 
c  Pressure     0.11418E+00    1053   0.81345E-02   0.23419E-01 0.10850E+00 
c  k            0.57904E+00     170   0.94993E-04   0.13547E-02 0.16637E+01 
c  epsilon      0.36791E+04     101   0.10014E-02   0.28588E+07 0.24448E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0033964                            12
a  epsilon                 -281.03                            15
a  Local Time Step      1.1808e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.8284          14.159          1.6381         0.39314
v  Velocity[Y]              -11.21          16.423          1.3655         0.93899
v  Velocity[Z]             -15.781          11.122         -1.0562       -0.014891
v  ǁVelocityǁ             0.013203          19.331          6.2918           7.457
v  Pressure                 -28307      2.0505e+05      1.3395e+05      1.0744e+05
v  k                    4.9527e-07          5.4194        0.071962          0.1113
v  epsilon               0.0054008      1.3019e+06          1779.5           59.08
v  TurbVisc             1.6168e-12          0.5151       0.0035701        0.050347
v  CourantNb               0.48881      8.4689e+05          406.39          82.211
v  FourierNb               0.22705      2.3653e+06          219.07          3.4631
v  total_pressure       4.7169e+05      7.0505e+05      6.3395e+05      6.0744e+05
v  Local Time Step            0.01        0.057375            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6303      2.8216e+06          625.47          85.675


 TIME FOR THE TIME STEP              757:        0.19294E+03

===============================================================


 INSTANT    0.758000000E+02   TIME STEP NUMBER             7Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.218281363E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160418E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17027E+02 0.55410E+01
   Friction velocity        uet   :  0.32745E-01 0.40060E+02
   Friction velocity        uk    :  0.37009E-01 0.40060E+02
   Dimensionless distance   yplus :  0.21971E-02 0.24879E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13535
   Nb of faces within the viscous sub-layer     :      11312
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48899E+01     644   0.24023E+00   0.10862E+02 0.42857E+01 
c  Velocity[X]                                      0.28400E+01 
c  Velocity[Y]                                      0.52913E+01 
c  Velocity[Z]                                      0.27305E+01 
c  Pressure     0.11121E+00     940   0.79680E-02   0.22835E-01 0.48492E-01 
c  k            0.57890E+00     167   0.67717E-04   0.97588E-03 0.14123E+01 
c  epsilon      0.35468E+04      97   0.82320E-03   0.14435E+07 0.18431E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00041781                            17
a  epsilon                  -204.6                            46
a  Local Time Step      1.2971e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6412          14.037          1.6293         0.39477
v  Velocity[Y]             -11.271          15.815          1.3313         0.94084
v  Velocity[Z]             -16.467          11.554          -1.063      Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.218281363E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160418E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17027E+02 0.55410E+01
   Friction velocity        uet   :  0.32745E-01 0.40060E+02
   Friction velocity        uk    :  0.37009E-01 0.40060E+02
   Dimensionless distance   yplus :  0.21971E-02 0.24879E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13535
   Nb of faces within the viscous sub-layer     :      11312
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
--------------------------------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.218281363E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160418E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17027E+02 0.55410E+01
   Friction velocity        uet   :  0.32745E-01 0.40060E+02
   Friction velocity        uk    :  0.37009E-01 0.40060E+02
   Dimensionless distance   yplus :  0.21971E-02 0.24879E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13535
   Nb of faces within the viscous sub-layer     :      11312
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48899E+01     644   0.24023E+00   0.10862E+02 0.42857E+01 
c  Velocity[X]                                      0.28400E+01 
c  Velocity[Y]                                      0.52913E+01 
c  Velocity[Z]                                      0.27305E+01 
c  Pressure     0.11121E+00     940   0.79680E-02   0.22835E-01 0.48492E-01 
c  k            0.57890E+00     167   0.67717E-04   0.97588E-03 0.14123E+01 
c  epsilon      0.35468E+04      97   0.82320E-03   0.14435E+07 0.18431E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00041781                            17
a  epsilon                  -204.6                            46
a  Local Time Step      1.2971e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  ---v  Velocity[Z]             -18.327          10.575         -1.0905       -0.013862
v  ǁVelocityǁ             0.010983          21.029          6.3498          7.4648
v  Pressure                 -28280      2.0502e+05      1.3392e+05      1.0743e+05
v  k                    5.9048e-07          5.3341        0.072018         0.11123
v  epsilon               0.0054829      1.2631e+06          1752.8          58.971
v  TurbVisc             1.8237e-12          0.5151       0.0035669        0.050327
v  CourantNb               0.24239      8.3022e+05          400.09          82.064
v  FourierNb               0.22617      2.3653e+06          219.04          3.4635
v  total_pressure       4.7172e+05      7.0502e+05      6.3392e+05      6.0743e+05
v  Local Time Step            0.01        0.048784            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6632      2.6761e+06          619.13          85.527


 TIME FOR THE TIME STEP              760:        0.16884E+03

===============================================================


 INSTANT    0.761000000E+02   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         0.239560823E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160826E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17199E+02 0.55410E+01
   Friction velocity        uet   :  0.41811E-01 0.22748E+02
   Friction velocity        uk    :  0.46017E-01 0.22748E+02
   Dimensionless distance   yplus :  0.22179E-02 0.24879E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13538
   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
-------------v  Velocity[Z]             -18.327          10.575         -1.0905       -0.013862
v  ǁVelocityǁ             0.010983          21.029          6.3498          7.4648
v  Pressure                 -28280      2.0502e+05      1.3392e+05      1.0743e+05
v  k                    5.9048e-07          5.3341        0.072018         0.11123
v  epsilon               0.0054829      1.2631e+06          1752.8          58.971
v  TurbVisc             1.8237e-12          0.5151       0.0035669        0.050327
v  CourantNb               0.24239      8.3022e+05          400.09          82.064
v  FourierNb               0.22617      2.3653e+06          219.04          3.4635
v  total_pressure       4.7172e+05      7.0502e+05      6.3392e+05      6.0743e+05
v  Local Time Step            0.01        0.048784            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6632      2.6761e+06          619.13          85.527


 TIME FOR THE TIME STEP              760:        0.17261E+03

===============================================================


 INSTANT    0.761000000E+02   TIME STEP NUMBER             761
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet         v  Velocity[Z]             -18.327          10.575         -1.0905       -0.013862
v  ǁVelocityǁ             0.010983          21.029          6.3498          7.4648
v  Pressure                 -28280      2.0502e+05      1.3392e+05      1.0743e+05
v  k                    5.9048e-07          5.3341        0.072018         0.11123
v  epsilon               0.0054829      1.2631e+06          1752.8          58.971
v  TurbVisc             1.8237e-12          0.5151       0.0035669        0.050327
v  CourantNb               0.24239      8.3022e+05          400.09          82.064
v  FourierNb               0.22617      2.3653e+06          219.04          3.4635
v  total_pressure       4.7172e+05      7.0502e+05      6.3392e+05      6.0743e+05
v  Local Time Step            0.01        0.048784            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6632      2.6761e+06          619.13          85.527


 TIME FOR THE TIME STEP              760:        0.16594E+03

===============================================================


 INSTANT    0.761000000E+02   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         0.239560823E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160826E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17199E+02 0.55410E+01
   Friction velocity        uet   :  0.41811E-01 0.22748E+02
   Friction velocity        uk    :  0.46017E-01 0.22748E+02
   Dimensionless distance   yplus :  0.22179E-02 0.24879E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13538
   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     0.48972E+01     642   0.24523E+00   0.11309E+02 0.43742E+01 
c  Velocity[X]                                      0.31726E+01 
c  Velocity[Y]                                      0.55474E+01 
c  Velocity[Z]                                      0.25890E+01 
c  Pressure     0.11258E+00     960   0.78395E-02   0.23123E-01 0.65101E-01 
c  k            0.57917E+00     160   0.96189E-04   0.15299E-02 0.17675E+01 
c  epsilon      0.40456E+04      93   0.82986E-03   0.23892E+07 0.22041E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00034591                            33
a  epsilon                 -24.712                            45
a  Local Time Step      1.1829e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7034          14.163          1.6386         0.39326
v  Velocity[Y]             -11.086          16.168          1.3871         0.93976
v  Velocity[Z]             -15.283          11.558         -1.0714       -0.014976
v  ǁVelocityǁ            0.0086723          19.095          6.3039          7.4568
v  Pressure                 -28324      2.0511e+05      1.3399e+05      1.0749e+05
v  k                    5.8888e-07          5.4169        0.072279          0.1113
v  epsilon               0.0057339      1.3009e+06          1792.3          59.203
v  TurbVisc             1.5703e-12          0.5151       0.0035752        0.050328
v  CourantNb               0.11213       8.454e+05          406.49          82.207
v  FourierNb               0.22613      2.3653e+06          219.07          3.4627
v  total_pressure       4.7168e+05      7.0511e+05      6.3399e+05      6.0749e+05
v  Local Time Step            0.01        0.053662            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4902      2.8806e+06          625.57          85.669


 TIME FOR THE TIME STEP              761:        0.18459E+03

===============================================================


 INSTANT    0.762000000E+02   TIME STEP NUMBER             762
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
-----------------------------------------------------------------------------
c  Velocity     0.49002E+01     641   0.24510E+00   0.11930E+02 0.44911E+01 
c  Velocity[X]                                      0.31207E+01 
c  Velocity[Y]                                      0.65867E+01 
c  Velocity[Z]                                      0.22231E+01 
c  Pressure     0.10462E+00     993   0.73737E-02   0.21490E-01 0.65696E-01 
c  k            0.57923E+00     159   0.73283E-04   0.13022E-02 0.16306E+01 
c  epsilon      0.40489E+04     102   0.97219E-03   0.20092E+07 0.20408E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0014302                            21
a  epsilon                 -156.57                            48
a  Local Time Step      1.0946e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5876          14.123           1.647         0.39361
v  Velocity[Y]               -11.1          15.962          1.3395         0.94123
v  Velocity[Z]             -18.234           10.72         -1.0452       -0.014674
v  ǁVelocityǁ            0.0097206          20.936           6.261          7.4607
v  Pressure                 ------------------------------------------------------------------------------
c  Velocity     0.49002E+01     641   0.24510E+00   0.11930E+02 0.44911E+01 
c  Velocity[X]                                      0.31207E+01 
c  Velocity[Y]                                      0.65867E+01 
c  Velocity[Z]                                      0.22231E+01 
c  Pressure     0.10462E+00     993   0.73737E-02   0.21490E-01 0.65696E-01 
c  k            0.57923E+00     159   0.73283E-04   0.13022E-02 0.16306E+01 
c  epsilon      0.40489E+04     102   0.97219E-03   0.20092E+07 0.20408E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0014302                            21
a  epsilon                 -156.57                            48
a  Local Time Step      1.0946e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5876          14.123           1.647         0.39361
v  Velocity[Y]               -11.1          15.962          1.3395         0.94123
v  Velocity[Z]             -18.234           10.72         -1.0452       -0.014674
v  ǁVelocityǁ            0.0097206          20.936           6.261          7.4607
v  Pressure                 -28412      2.0505e+05      1.3389e+05      1.0742e+05
v  k                    1.6375e-07          5.6014        0.071263         0.11138
v  epsilon              0.00019608        1.36e+06          1761.1          58.796
v  TurbVisc             1.8703e-12          0.5151       0.0035837        0.050337
v  CourantNb              0.011872      9.1356e+05          403.39          82.003
v  FourierNb               0.22637      2.3653e+06          219.09          3.4636
v  total_pressure       4.7159e+05      7.0505e+05      6.3389e+05      6.0742e+05
v  Local Time Step            0.01        0.059028            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.799      3.0392e+06          622.48          85.466


 TIME FOR THE TIME STEP              762:        0.17634E+03

===============================================================


 INSTANT    0.763000000E+02   TIME STEP NUMBER             763
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
----------------------------------------------Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160852E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17162E+02 0.55410E+01
   Friction velocity        uet   :  0.39297E-01 0.47651E+02
   Friction velocity        uk    :  0.37785E-01 0.47651E+02
   Dimensionless distance   yplus :  0.38264E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13556
   Nb of faces within the viscous sub-layer     :      11098
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48936E+01     643   0.24006E+00   0.12762E+02 0.46431E+01 
c  Velocity[X]                                      0.34585E+01 
c  Velocity[Y]                                      0.72605E+01 
c  Velocity[Z]                                      0.20428E+01 
c  Pressure     0.10570E+00     906   0.73534E-02   0.21697E-01 0.40260E-01 
c  k            0.57934E+00     180   0.70600E-04   0.98519E-03 0.14180E+01 
c  epsilon      0.39612E+04     101   0.53308E-03   0.87181E+06 0.13749E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0008952                            12
a  epsilon                 -24.698                            19
a  Local Time Step      1.1821e-08                        281788


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5917          14.117          1.6349         0.39325
v  Velocity[Y]             -11.192          15.786          1.4059         0.93851
v  Velocity[Z]               -15.7           10.92         -1.0721       -0.013983
v  ǁVelocityǁ            0.0022165          18.906          6.3422          7.4637
v  Pressure                 -28437      2.0505e+05      1.3388e+05      1.0743e+05
v  k                    2.9413e-07          5.4006        0.071953          0.1115
v  epsilon               0.0024567      1.2848e+06    Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160852E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17162E+02 0.55410E+01
   Friction velocity        uet   :  0.39297E-01 0.47651E+02
   Friction velocity        uk    :  0.37785E-01 0.47651E+02
   Dimensionless distance   yplus :  0.38264E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13556
   Nb of faces within the viscous sub-layer     :      11098
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48936E+01     643   0.24006E+00   0.12762E+02 0.46431E+01 
c  Velocity[X]                       Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160852E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17162E+02 0.55410E+01
   Friction velocity        uet   :  0.39297E-01 0.47651E+02
   Friction velocity        uk    :  0.37785E-01 0.47651E+02
   Dimensionless distance   yplus :  0.38264E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13556
   Nb of faces within the viscous sub-layer     :      11098
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48936E+01     643   0.24006E+00   0.12762E+02 0.46431E+01 
c  Velocity[X]                                      0.34585E+01 
c  Velocity[Y]                                      0.72605E+01 
c  Velocity[Z]                                      0.20428E+01 
c  Pressure     0.10570E+00     906   0.73534E-02   0.21697E-01 0.40260E-01 
c  k            0.57934E+00     180   0.70600E-04   0.98519E-03 0.14180E+01 
c  epsilon      0.39612E+04     101   0.53308E-03   0.87181E+06 0.13749E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0008952                            12
a  epsilon                 -24.698                            19
a  Local Time Step      1.1821e-08                        281788


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5917          14.117          1.6349         0.39325
v  Velocity[Y]             -11.192          15.786          1.4059         0.93851
v  Velocity[Z]               -15.7           10.92         -1.0721       -0.013983
v  ǁVelocityǁ            0.0022165     v  epsilon              0.00032073      1.2891e+06          1802.4          59.404
v  TurbVisc              1.571e-12          0.5151       0.0035748        0.050364
v  CourantNb               0.46052      8.4185e+05          406.02          82.179
v  FourierNb               0.22776      2.3653e+06          219.06          3.4631
v  total_pressure       4.7157e+05      7.0518e+05      6.3397e+05      6.0747e+05
v  Local Time Step            0.01        0.078566        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4394      2.9674e+06          625.08          85.642


 TIME FOR THE TIME STEP              765:        0.18916E+03

===============================================================


 INSTANT    0.766000000E+02   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         0.743892297E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160434E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16856E+02 0.55409E+01
   Friction velocity        uet   :  0.45610E-01 0.57297E+02
   Friction velocity        uk    :  0.47790E-01 0.57297E+02
   Dimensionless distance   yplus :  0.33975E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13481
   Nb of faces within the viscous sub-layer     :      11151
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48917E+01     649   0.23961E+00   0.12133E+02 0.45294E+01 
c  Velocity[X]                                      0.34317E+01 
c  Velocity[Y]                                      0.63796E+01 
c  Velocity[Z]                                      0.23219E+0v  epsilon              0.00032073      1.2891e+06          1802.4          59.404
v  TurbVisc              1.571e-12          0.5151       0.0035748        0.050364
v  CourantNb               0.46052      8.4185e+05          406.02          82.179
v  FourierNb               0.22776      2.3653e+06          219.06          3.4631
v  total_pressure       4.7157e+05      7.0518e+05      6.3397e+05      6.0747e+05
v  Local Time Step            0.01        0.078566        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4394      2.9674e+06          625.08          85.642


 TIME FOR THE TIME STEP              765:        0.18028E+03

===============================================================


 INSTANT    0.766000000E+02   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         0.743892297E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160434E+01
Free inlet               13 v  epsilon              0.00032073      1.2891e+06          1802.4          59.404
v  TurbVisc              1.571e-12          0.5151       0.0035748        0.050364
v  CourantNb               0.46052      8.4185e+05          406.02          82.179
v  FourierNb               0.22776      2.3653e+06          219.06          3.4631
v  total_pressure       4.7157e+05      7.0518e+05      6.3397e+05      6.0747e+05
v  Local Time Step            0.01        0.078566        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4394      2.9674e+06          625.08          85.642


 TIME FOR THE TIME STEP              765:        0.18790E+03

===============================================================


 INSTANT    0.766000000E+02   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         0.743892297E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160434E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16856E+02 0.55409E+01
   Friction velocity        uet   :  0.45610E-01 0.57297E+02
   Friction velocity        uk    :  0.47790E-01 0.57297E+02
   Dimensionless distance   yplus :  0.33975E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13481
   Nb of faces within the viscous sub-layer     :      11151
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48917E+01     649   0.23961E+00   0.12133E+02 0.45294E+01 
c  Velocity[X]                                      0.34317E+01 
c  Velocity[Y]                                      0.63796E+01 
c  Velocity[Z]                                      0.23219E+01 
c  Pressure     0.10768E+00     778   0.76458E-02   0.22110E-01 0.34333E-01 
c  k            0.57933E+00     161   0.69904E-04   0.12413E-02 0.15919E+01 
c  epsilon      0.40710E+04     103   0.53862E-03   0.16458E+07 0.18599E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0026763                            20
a  epsilon                  -181.9                            56
a  Local Time Step      1.1401e-08                        281786


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6284          14.172          1.6433         0.39387
v  Velocity[Y]             -11.157          15.906          1.3221         0.94103
v  Velocity[Z]             -14.898          10.893         -1.0159        -0.01428
v  ǁVelocityǁ             0.014229          18.909           6.263          7.4605
v  Pressure                 -28441      2.0519e+05      1.3395e+05      1.0745e+05
v  k                    2.8555e-07          5.5775        0.070746         0.11144
v  epsilon              0.00027513       1.351e+06          1723.5          58.737
v  TurbVisc              2.145e-12          0.5151       0.0035812        0.050366
v  CourantNb               0.14451      8.7715e+05          403.01          81.946
v  FourierNb               0.22771      2.3653e+06          219.07          3.4645
v  total_pressure       4.7156e+05      7.0519e+05      6.3395e+05      6.0745e+05
v  Local Time Step            0.01        0.086423        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6208      3.0028e+06          622.09           85.41


 TIME FOR THE TIME STEP              766:        0.17825E+03

===============================================================


 INSTANT    0.767000000E+02   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         0.144393073E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3  c  Velocity[Z]                                      0.25448E+01 
c  Pressure     0.10172E+00     944   0.71892E-02   0.20885E-01 0.44005E-01 
c  k            0.57924E+00     165   0.71976E-04   0.10411E-02 0.14580E+01 
c  epsilon      0.39549E+04     113   0.76752E-03   0.13919E+07 0.17670E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00055516                            13
a  epsilon                 -497.48                            21
a  Local Time Step      1.2648e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7114          14.032          1.6331         0.39493
v  Velocity[Y]             -11.182          16.304          1.3381         0.93987
v  Velocity[Z]             -18.194          11.636         -1.0468       -0.013777
v  ǁVelocityǁ             0.014952          20.985          6.3024          7.4591
v  Pressure                 -28385      2.0524e+05      1.3401e+05       1.075e+05
v  k                    2.5554e-07          5.3523        0.070527         0.11142
v  epsilon              0.00079205      1.2676e+06          1673.7          58.828
v  TurbVisc             1.7908e-12          0.5151       0.003574c  Velocity[Z]                                      0.25448E+01 
c  Pressure     0.10172E+00     944   0.71892E-02   0.20885E-01 0.44005E-01 
c  k            0.57924E+00     165   0.71976E-04   0.10411E-02 0.14580E+01 
c  epsilon      0.39549E+04     113   0.76752E-03   0.13919E+07 0.17670E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00055516                            13
a  epsilon                 -497.48                            21
a  Local Time Step      1.2648e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7114          14.032          1.6331         0.39493
v  Velocity[Y]             -11.182          16.304          1.3381         0.93987
v  Velocity[Z]             -18.194          11.636         -1.0468       -0.013777
v  ǁVelocityǁ             0.014952          20.985          6.3024          7.4591
v  Pressure                 -28385      2.0524e+05      1.3401e+05       1.075e+05
v  k                    2.5554e-07          5.3523        0.070527         0.11142
v  epsilon              0.00079205      1.2676e+06          1673.7          58.828
v  TurbVisc             1.7908e-12          0.5151       0.0035742        0.050363
v  CourantNb             0.0052266      7.9064e+05           396.4          81.984
v  FourierNb               0.22763      2.3653e+06          219.05          3.4632
v  total_pressure       4.7161e+05      7.0524e+05      6.3401e+05       6.075e+05
v  Local Time Step            0.01        0.095065        0.010001        0.010007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5809      2.7082e+06          615.45          85.447


 TIME FOR THE TIME STEP              767:        0.18730E+03

===============================================================


 INSTANT    0.768000000E+02   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         0.288535715E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0       Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16720E+02 0.55410E+01
   Friction velocity        uet   :  0.45503E-01 0.55065E+02
   Friction velocity        uk    :  0.45359E-01 0.55065E+02
   Dimensionless distance   yplus :  0.10004E-02 0.24879E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13525
   Nb of faces within the viscous sub-layer     :      11054
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48899E+01     617   0.24023E+00   0.11139E+02 0.43413E+01 
c  Velocity[X]                                      0.33734E+01 
c  Velocity[Y]                                      0.49866E+01 
c  Velocity[Z]                                      0.27792E+01 
c  Pressure     0.10407E+00     958   0.72750E-02   0.21353E-01 0.46350E-01 
c  k            0.57922E+00     159   0.95569E-04   0.13760E-02 0.16762E+01 
c  epsilon      0.40024E+04      99   0.98200E-03   0.22240E+07 0.21525E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0018096                            38
a  epsilon                 -5.6408                            71
a  Local Time Step       1.109e-08                        281779


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7336          14.196          1.6397          0.3931
v  Velocity[Y]             -11.145          16.308           1.373         0.93965
v  Velocity[Z]             -19.302           12.16         -1.0601       -0.015142
v  ǁVelocityǁ            0.0071291          22.023          6.3133          7.4564
v  Pressure                 -28432      2.0534e+05      1.3412e+05      1.0756e+05
v  k                    7.0308e-09          5.3062        0.072137         0.11139
v  epsilon               0.0037139      1.2622e+06          1772.9          59.191
v  TurbVisc             1.7405e-12          0.5151       0.0035761        0.050351
v  CourantNb               0.11265      9.0174e+05          404.24          82.117
v  FourierNb               0.22735      2.3653e+06          2Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16720E+02 0.55410E+01
   Friction velocity        uet   :  0.45503E-01 0.55065E+02
   Friction velocity        uk    :  0.45359E-01 0.55065E+02
   Dimensionless distance   yplus :  0.10004E-02 0.24879E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13525
   Nb of faces within the viscous sub-layer     :      11054
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48899E+01     617   0.24023E+00   0.11139E+02 0.43413E+01 
c  Velocity[X]                                      0.33734E+01 
c  Velocity[Y]                                      0.49866E+01 
c  Velocity[Z]                                      0.27792E+01 
c  Pressure     0.10407E+00     958   0.72750E-02   0.21353E-01 0.46350E-01 
c  k            0.579Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16720E+02 0.55410E+01
   Friction velocity        uet   :  0.45503E-01 0.55065E+02
   Friction velocity        uk    :  0.45359E-01 0.55065E+02
   Dimensionless distance   yplus :  0.10004E-02 0.24879E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13525
   Nb of faces within the viscous sub-layer     :      11054
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48899E+01     617   0.24023E+00   0.11139E+02 0.43413E+01 
c  Velocity[X]                                      0.33734E+01 
c  Velocity[Y]                                      0.49866E+01 
c  Velocity[Z]                                      0.27792E+01 
c  Pressure     0.10407E+00     958   0.72750E-02   0.21353E-01 0.46350E-01 
c  k            0.57922E+00     159   0.95569E-04   0.13760E-02 0.16762E+01 
c  epsilon      0.40024E+04      99   0.98200E-03   0.22240E+07 0.21525E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0018096                            38
a  epsilon                 -5.6408                            71
a  Local Time Step       1.109e-08                        281779


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7336          14.196          1.6397          0.3931
v  Velocity[Y]             -11.145          16.308           1.373         0.93965
v  Velocity[Z]             -19.302           12.16         -1.0601       -0.015142
v  ǁVelocityǁ            0.0071291          22.023          6.3133          7.4564
v  Pressure                 -28432      2.0534e+05      1.3412e+05      1.0756e+05
v  k                    7.0308e-09          5.3062        0.072137         0.11139
v  epsilon               0.0037139     v  FourierNb               0.22715      2.3653e+06          219.07          3.4642
v  total_pressure       4.7156e+05      7.0537e+05      6.3413e+05      6.0759e+05
v  Local Time Step            0.01          0.0532            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6443      2.9164e+06          623.42          85.475


 TIME FOR THE TIME STEP              770:        0.17906E+03

===============================================================


 INSTANT    0.771000000E+02   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         0.146130821E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160415E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17182E+02 0.55410E+01
   Friction velocity        uet   :  0.39804E-01 0.54536E+02
   Friction velocity        uk    :  0.46176E-01 0.54536E+02
   Dimensionless distance   yplus :  0.38597E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13529
   Nb of faces within the viscous sub-layer     :      11182
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49001E+01     644   0.24791E+00   0.10463E+02 0.42065E+01 
c  Velocity[X]                                      0.32174E+01 
c  Velocity[Y]                                      0.47833E+01 
c  Velocity[Z]                                      0.24622E+01 
c  Pressure     0.10535E+00     826   0.74336E-02   0.21615E-01 0.22114E-01 
c  k            0.57919E+00     164   0.69038E-04   0.95844E-03 0.13989E+01 
c  epsilon      0.39781E+04     114   0.80129E-03   0.13534E+07 0.17178E+02 
---------------v  FourierNb               0.22715      2.3653e+06          219.07          3.4642
v  total_pressure       4.7156e+05      7.0537e+05      6.3413e+05      6.0759e+05
v  Local Time Step            0.01          0.0532            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6443      2.9164e+06          623.42          85.475


 TIME FOR THE TIME STEP              770:        0.17980E+03

===============================================================


 INSTANT    0.771000000E+02   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         0.146130821E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160415E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------v  FourierNb               0.22715      2.3653e+06          219.07          3.4642
v  total_pressure       4.7156e+05      7.0537e+05      6.3413e+05      6.0759e+05
v  Local Time Step            0.01          0.0532            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6443      2.9164e+06          623.42          85.475


 TIME FOR THE TIME STEP              770:        0.18100E+03

===============================================================


 INSTANT    0.771000000E+02   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         0.146130821E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160415E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17182E+02 0.55410E+01
   Friction velocity        uet   :  0.39804E-01 0.54536E+02
   Friction velocity        uk    :  0.46176E-01 0.54536E+02
   Dimensionless distance   yplus :  0.38597E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13529
   Nb of faces within the viscous sub-layer     :      11182
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49001E+01     644   0.24791E+00   0.10463E+02 0.42065E+01 
c  Velocity[X]                                      0.32174E+01 
c  Velocity[Y]                                      0.47833E+01 
c  Velocity[Z]                                      0.24622E+01 
c  Pressure     0.10535E+00     826   0.74336E-02   0.21615E-01 0.22114E-01 
c  k            0.57919E+00     164   0.69038E-04   0.95844E-03 0.13989E+01 
c  epsilon      0.39781E+04     114   0.80129E-03   0.13534E+07 0.17178E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00019263                             9
a  epsilon                  -370.5                            21
a  Local Time Step      1.2209e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6455          13.988          1.6432         0.39409
v  Velocity[Y]             -11.242          16.389          1.3405         0.94078
v  Velocity[Z]             -19.259          9.6609         -1.0676       -0.014675
v  ǁVelocityǁ             0.016068          21.999          6.2974          7.4598
v  Pressure                 -28459      2.0534e+05       1.341e+05      1.0758e+05
v  k                    5.2903e-07          5.5567         0.07098         0.11143
v  epsilon               0.0065936      1.2868e+06          1715.4          58.935
v  TurbVisc             1.9182e-12          0.5151       0.0035828        0.050353
v  CourantNb               0.19486       8.191e+05          397.47           82.02
v  FourierNb               0.22708      2.3653e+06          219.06          3.4632
v  total_pressure       4.7154e+05      7.0534e+05       6.341e+05      6.0758e+05
v  Local Time Step            0.01         0.05852            0.01        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6698      2.6992e+06          616.53          85.483


 TIME FOR THE TIME STEP              771:        0.18398E+03

===============================================================


 INSTANT    0.772000000E+02   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        -0.171048222E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160825E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
----------------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0020075                            33
a  epsilon                  -17.49                            23
a  Local Time Step      1.1242e-08                        281786


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5279          14.061          1.6367         0.39367
v  Velocity[Y]             -11.218          15.822          1.3911          0.9393
v  Velocity[Z]             -15.261          11.772         -1.0768       -0.014307
v  ǁVelocityǁ             0.025672          18.753          6.3114          7.4613
v  Pressure                 -28488      2.0533e+05       1.341e+05      1.0757e+05
v  k                    9.8136e-08          5.7106        0.071107         0.11142
v  epsilon               0.0059971      1.3027e+06            1705              59
v  TurbVisc             1.5679e-12          0.5151       0.0035755        0.050352
v  CourantNb             0.0089638      8.8956e+05          399.58          82.111
v  FourierNb               0.22705      2.3653e+06          219.06          3.4628
v  total_pressure       4.7151e+05      7.0533e+05       6.341e+05      6.0757e+05
v  Local Time Step           -----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0020075                            33
a  epsilon                  -17.49                            23
a  Local Time Step      1.1242e-08                        281786


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5279          14.061          1.6367         0.39367
v  Velocity[Y]             -11.218          15.822          1.3911          0.9393
v  Velocity[Z]             -15.261          11.772         -1.0768       -0.014307
v  ǁVelocityǁ             0.025672          18.753          6.3114          7.4613
v  Pressure                 -28488      2.0533e+05       1.341e+05      1.0757e+05
v  k                    9.8136e-08          5.7106        0.071107         0.11142
v  epsilon               0.0059971      1.3027e+06            1705              59
v  TurbVisc             1.5679e-12          0.5151       0.0035755        0.050352
v  CourantNb             0.0089638      8.8956e+05          399.58          82.111
v  FourierNb               0.22705      2.3653e+06          219.06          3.4628
v  total_pressure       4.7151e+05      7.0533e+05       6.341e+05      6.0757e+05
v  Local Time Step            0.01        0.046712            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6584      2.8202e+06          618.64          85.573


 TIME FOR THE TIME STEP              772:        0.16446E+03

===============================================================


 INSTANT    0.773000000E+02   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         0.206735231E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160805E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefi------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17118E+02 0.55409E+01
   Friction velocity        uet   :  0.24808E-01 0.43684E+02
   Friction velocity        uk    :  0.24788E-01 0.43684E+02
   Dimensionless distance   yplus :  0.32098E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13547
   Nb of faces within the viscous sub-layer     :      11163
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49020E+01     669   0.24433E+00   0.12512E+02 0.45983E+01 
c  Velocity[X]                                      0.34165E+01 
c  Velocity[Y]                                      0.66842E+01 
c  Velocity[Z]                                      0.24116E+01 
c  Pressure     0.10722E+00     501   0.74823E-02   0.21978E-01 0.18141E-01 
c  k            0.57924E+00     167   0.62439E-04   0.10068E-02 0.14337E+01 
c  epsilon      0.41157E+04      96   0.66070E-03   0.15091E+07 0.17463E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0017898                            30
a  epsilon                 -99.271                            60
a  Local Time Step      1.2395e-08                        281781


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6989          14.069          1.6337         0.39311
v  Velocity[Y]             -11.163          15.928          1.3322         0.94068
v  Velocity[Z]             -16.862          10.772         -1.0247       -0.015305
v  ǁVelocityǁ             0.014531          19.665          6.2714          7.4603
v  Pressure                 -28466      2.0544e+05      1.3415e+05      1.0761e+05
v  k                    4.7733e-07           5.969        0.071292         0.11142
v  epsilon              0.00024469      1.4056e+06          1766.1          58.971
v  TurbVisc             1.9237e-12          0.5151       0.0035766        0.050353
v  CourantNb              0.054141      8.0675e+05          404.52          82.098
v  FourierNb               0.22705      2.3653e+06          219.07           3.464
v  total_pressure       4.7153e+05      7.0544e+05      6.3415e+05      6.0761e+05
v  Local Time Step            0.01         0.05599            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               mi------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17118E+02 0.55409E+01
   Friction velocity        uet   :  0.24808E-01 0.43684E+02
   Friction velocity        uk    :  0.24788E-01 0.43684E+02
   Dimensionless distance   yplus :  0.32098E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13547
   Nb of faces within the viscous sub-layer     :      11163
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49020E+01     669   0.24433E+00   0.12512E+02 0.45983E+01 
c  Velocity[X]                                      0.34165E+01 
c  Velocity[Y]                                      0.66842E+01 
c  Velocity[Z]                                      0.24116E+01 
c  Pressure     0.10722E+00     501   0.74823E-02   0.21978E-01 0.18141E-01 
c  k            0.57924E+00     167   0.62439E-04   0.10068E-02 0.14337E+01 
c  epsilon      0.41157E+04      96   0.66070E-03   0.15091E+07 0.17463E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     ----------------------------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17118E+02 0.55409E+01
   Friction velocity        uet   :  0.24808E-01 0.43684E+02
   Friction velocity        uk    :  0.24788E-01 0.43684E+02
   Dimensionless distance   yplus :  0.32098E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13547
   Nb of faces within the viscous sub-layer     :      11163
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49020E+01     669   0.24433E+00   0.12512E+02 0.45983E+01 
c  Velocity[X]                                      0.34165E+01 
c  Velocity[Y]                                      0.66842E+01 
c  Velocity[Z]                                      0.24116E+01 
c  Pressure     0.10722E+00     501   0.74823E-02   0.21978E-01 0.18141E-01 
c  k            0.57924E+00     167   0.62439E-04   0.10068E-02 0.14337E+01 
c  epsilon      0.41157E+04      96   0.66070E-03   0.15091E+07 0.17463E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0017898                            30
a  epsilon                 -99.271                            60
a  Local Time Step      1.2395e-08                        281781


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6989          14.069          1.6337         0.39311
v  Velocity[Y]             -11.163          15.928          1.3322         0.94068
v  Velocity[Z]             -16.862          10.772         -1.0247       -0.015305
v  ǁVelocityǁ             0.014531          19.665          6.2714          7.4603
v  Pressure                 -28466      2.0544e+05      1.3415e+05      1.0761e+05
v  k                    4.7733e-07           5.969        0.071292         0.11142
v  epsilon              0.00024469      1.4056e+06          1766.1          58.971
v  TurbVisc             1.9237e-12          0.5151       0.0035766        0.050353
v  CourantNb              0.054141      8.0675e+05          404.52          82.098
v  FourierNb               0.22705      2.3653e+06          219.07           3.464
v  total_pressure 
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5989      2.6806e+06          617.72          85.424


 TIME FOR THE TIME STEP              775:        0.17905E+03

===============================================================


 INSTANT    0.776000000E+02   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        -0.133004393E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160838E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16780E+02 0.55409E+01
   Friction velocity        uet   :  0.36456E-01 0.26511E+02
   Friction velocity        uk    :  0.36352E-01 0.26511E+02
   Dimensionless distance   yplus :  0.33738E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13514
   Nb of faces within the viscous sub-layer     :      11123
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48906E+01     645   0.23661E+00   0.12404E+02 0.45785E+01 
c  Velocity[X]                                      0.33800E+01 
c  Velocity[Y]                                      0.65148E+01 
c  Velocity[Z]                                      0.25095E+01 
c  Pressure     0.10371E+00     810   0.75080E-02   0.21279E-01 0.36749E-01 
c  k            0.57920E+00     171   0.68755E-04   0.90865E-03 0.13621E+01 
c  epsilon      0.39379E+04      94   0.44524E-03   0.87838E+06 0.14043E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k        
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5989      2.6806e+06          617.72          85.424


 TIME FOR THE TIME STEP              775:        0.17230E+03

===============================================================


 INSTANT    0.776000000E+02   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        -0.133004393E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160838E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
----------------------------------------------------------
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5989      2.6806e+06          617.72          85.424


 TIME FOR THE TIME STEP              775:        0.17203E+03

===============================================================


 INSTANT    0.776000000E+02   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        -0.133004393E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160838E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16780E+02 0.55409E+01
   Friction velocity        uet   :  0.36456E-01 0.26511E+02
   Friction velocity        uk    :  0.36352E-01 0.26511E+02
   Dimensionless distance   yplus :  0.33738E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13514
   Nb of faces within the viscous sub-layer     :      11123
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48906E+01     645   0.23661E+00   0.12404E+02 0.45785E+01 
c  Velocity[X]                                      0.33800E+01 
c  Velocity[Y]                                      0.65148E+01 
c  Velocity[Z]                                      0.25095E+01 
c  Pressure     0.10371E+00     810   0.75080E-02   0.21279E-01 0.36749E-01 
c  k            0.57920E+00     171   0.68755E-04   0.90865E-03 0.13621E+01 
c  epsilon      0.39379E+04      94   0.44524E-03   0.87838E+06 0.14043E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00045769                            24
a  epsilon                  -11.49                            26
a  Local Time Step      1.1264e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.586          14.093          1.6409         0.39301
v  Velocity[Y]              -11.25          15.974          1.3822         0.93859
v  Velocity[Z]             -15.078          10.058         -1.0542       -0.014155
v  ǁVelocityǁ             0.011022          18.795          6.3098          7.4606
v  Pressure                 -28502      2.0539e+05      1.3411e+05      1.0755e+05
v  k                    5.4633e-07          5.6805        0.070928         0.11141
v  epsilon               0.0046151      1.2984e+06          1675.7          58.923
v  TurbVisc             1.5506e-12          0.5151        0.003573        0.050352
v  CourantNb              0.070973      8.8776e+05          399.53          82.068
v  FourierNb               0.22711      2.3653e+06          219.04          3.4644
v  total_pressure        4.715e+05      7.0539e+05      6.3411e+05      6.0755e+05
v  Local Time Step            0.01        0.067748            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6564      2.8362e+06          618.57          85.533


 TIME FOR THE TIME STEP              776:        0.17998E+03

===============================================================


 INSTANT    0.777000000E+02   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         0.392040055E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160806E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
---------------------------------------------a  k                    -0.0015555                            16
a  epsilon                 -160.19                            40
a  Local Time Step      1.0562e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.8042          14.205          1.6415         0.39248
v  Velocity[Y]             -11.121           16.08          1.3814         0.93858
v  Velocity[Z]             -17.937           11.13         -1.0458       -0.015181
v  ǁVelocityǁ             0.002681          20.726          6.3422          7.4647
v  Pressure                 -28592      2.0539e+05      1.3413e+05      1.0755e+05
v  k                    4.3346e-08           5.593        0.071334         0.11142
v  epsilon              0.00046518      1.2779e+06            1717          58.999
v  TurbVisc             1.9619e-12          0.5151       0.0035746        0.050353
v  CourantNb               0.33589       9.468e+05          403.19          82.041
v  FourierNb                0.2272      2.3653e+06          219.05          3.4632
v  total_pressure       4.7141e+05      7.0539e+05      6.3413e+05      6.0755e+05
v  Local Time Step            0.01        0.074523            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6a  k                    -0.0015555                            16
a  epsilon                 -160.19                            40
a  Local Time Step      1.0562e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.8042          14.205          1.6415         0.39248
v  Velocity[Y]             -11.121           16.08          1.3814         0.93858
v  Velocity[Z]             -17.937           11.13         -1.0458       -0.015181
v  ǁVelocityǁ             0.002681          20.726          6.3422          7.4647
v  Pressure                 -28592      2.0539e+05      1.3413e+05      1.0755e+05
v  k                    4.3346e-08           5.593        0.071334         0.11142
v  epsilon              0.00046518      1.2779e+06            1717          58.999
v  TurbVisc             1.9619e-12          0.5151       0.0035746        0.050353
v  CourantNb               0.33589       9.468e+05          403.19          82.041
v  FourierNb                0.2272      2.3653e+06          219.05          3.4632
v  total_pressure       4.7141e+05      7.0539e+05      6.3413e+05      6.0755e+05
v  Local Time Step            0.01        0.074523            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6096      3.0724e+06          622.24          85.504


 TIME FOR THE TIME STEP              777:        0.17939E+03

===============================================================


 INSTANT    0.778000000E+02   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        -0.772073326E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160427E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
----------------------------------   Dimensionless distance   yplus :  0.34152E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13520
   Nb of faces within the viscous sub-layer     :      11106
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48976E+01     653   0.24374E+00   0.13416E+02 0.47636E+01 
c  Velocity[X]                                      0.38198E+01 
c  Velocity[Y]                                      0.70651E+01 
c  Velocity[Z]                                      0.25312E+01 
c  Pressure     0.10481E+00     507   0.74099E-02   0.21503E-01 0.29614E-01 
c  k            0.57929E+00     164   0.70457E-04   0.95210E-03 0.13942E+01 
c  epsilon      0.40658E+04      96   0.60037E-03   0.15662E+07 0.17945E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.3775e-05                             3
a  epsilon                 -15.915                            11
a  Local Time Step      1.1435e-08                        281786


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6257          14.053          1.6567         0.39315
v  Velocity[Y]             -11.395          16.324          1.3508         0.94046
v  Velocity[Z]             -15.942             9.8         -1.0509        -0.01487
v  ǁVelocityǁ             0.011503          19.387          6.2824          7.4596
v  Pressure                 -28594      2.0552e+05      1.3424e+05      1.0763e+05
v  k                    1.1054e-07          5.7432        0.071601         0.11148
v  epsilon               0.0068668      1.3291e+06          1763.3          59.142
v  TurbVisc             1.7016e-12          0.5151       0.0035882        0.050361
v  CourantNb               0.28867       8.745e+05          402.88          81.951
v  FourierNb               0.22742      2.3653e+06          219.08          3.4646
v  total_pressure       4.7141e+05      7.0552e+05      6.3424e+05      6.0763e+05
v  Local Time Step            0.01        0.090173            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5998      2.7184e+06          621.96          85.416


 TIME FOR THE TIME STEP              779:        0.16185E+03

===============================================================


 INSTANT    0.78   Dimensionless distance   yplus :  0.34152E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13520
   Nb of faces within the viscous sub-layer     :      11106
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48976E+01     653   0.24374E+00   0.13416E+02 0.47636E+01 
c  Velocity[X]                                      0.38198E+01 
c  Velocity[Y]                                      0.70651E+01 
c  Velocity[Z]                                      0.25312E+01 
c  Pressure     0.10481E+00     507   0.74099E-02   0.21503E-01 0.29614E-01 
c  k            0.57929E+00     164   0.70457E-04   0.95210E-03 0.13942E+01 
c  epsilon      0.40658E+04      96   0.60037E-03   0.15662E+07 0.17945E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.3775e-05                             3
a  epsilon                 -15.915                            11
a  Local Time Step      1.1435e-08                        281786


     Dimensionless distance   yplus :  0.34152E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13520
   Nb of faces within the viscous sub-layer     :      11106
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48976E+01     653   0.24374E+00   0.13416E+02 0.47636E+01 
c  Velocity[X]                                      0.38198E+01 
c  Velocity[Y]                                      0.70651E+01 
c  Velocity[Z]                                      0.25312E+01 
c  Pressure     0.10481E+00     507   0.74099E-02   0.21503E-01 0.29614E-01 
c  k            0.57929E+00     164   0.70457E-04   0.95210E-03 0.13942E+01 
c  epsilon      0.40658E+04      96   0.60037E-03   0.15662E+07 0.17945E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.3775e-05                             3
a  epsilon                 -15.915                            11
a  Local Time Step      1.1435e-08                        281786


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6257          14.053          1.6567         0.39315
v  Velocity[Y]             -11.395          16.324          1.3508         0.94046
v  Velocity[Z]             -15.942             9.8         -1.0509        -0.01487
v  ǁVelocityǁ             0.011503          19.387          6.2824          7.4596
v  Pressure                 -28594      2.0552e+05      1.3424e+05      1.0763e+05
v  k                    1.1054e-07          5.7432        0.071601         0.11148
v  epsilon               0.0068668      1.3291e+06          1763.3          59.142
v  TurbVisc             1.7016e-12          0.5151       0.0035882        0.050361
v  CourantNb               0.28867       8.745e+05          402.88          81.951
v  FourierNb               0.22742      2.3653e+06          219.08          3.4646
v  total_pressure       4.7141e+05      7.0552e+05      6.3424e+05      6.0763e+05
v  Local Time Step            0.01        0.090173            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
    INSTANT    0.781000000E+02   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         0.164596489E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160846E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16936E+02 0.55410E+01
   Friction velocity        uet   :  0.41345E-01 0.57012E+02
   Friction velocity        uk    :  0.46989E-01 0.57012E+02
   Dimensionless distance   yplus :  0.22840E-02 0.24879E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13570
   Nb of faces within the viscous sub-layer     :      11197
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48981E+01     628   0.24794E+00   0.13694E+02 0.48069E+01 
c  Velocity[X]                                      0.29869E+01 
c  Velocity[Y]                                      0.83381E+01 
c  Velocity[Z]                                      0.23688E+01 
c  Pressure     0.10928E+00     978   0.81100E-02   0.22386E-01 0.44069E-01 
c  k            0.57921E+00     172   0.72384E-04   0.11027E-02 0.15006E+01 
c  epsilon      0.39278E+04     100   0.62843E-03   0.11176E+07 0.15767E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0058854                            31
a  epsilon                 -150.35                            51
a  Local Time Step      1.1136e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  INSTANT    0.781000000E+02   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         0.164596489E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160846E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16936E+02 0.55410E+01
   Friction velocity        uet   :  0.41345E-01 0.57012E+02
   Friction velocity        uk    :  0.46989E-01 0.57012E+02
   Dimensionless distance   yplus :  0.22840E-02 0.24879E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13570
   Nb of faces INSTANT    0.781000000E+02   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         0.164596489E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160846E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16936E+02 0.55410E+01
   Friction velocity        uet   :  0.41345E-01 0.57012E+02
   Friction velocity        uk    :  0.46989E-01 0.57012E+02
   Dimensionless distance   yplus :  0.22840E-02 0.24879E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13570
   Nb of faces within the viscous sub-layer     :      11197
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48981E+01     628   0.24794E+00   0.13694E+02 0.48069E+01 
c  Velocity[X]                                      0.29869E+01 
c  Velocity[Y]                                      0.83381E+01 
c  Velocity[Z]                                      0.23688E+01 
c  Pressure     0.10928E+00     978   0.81100E-02   0.22386E-01 0.44069E-01 
c  k            0.57921E+00     172   0.72384E-04   0.11027E-02 0.15006E+01 
c  epsilon      0.39278E+04     100   0.62843E-03   0.11176E+07 0.15767E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0058854                            31
a  epsilon                 -150.35                            51
a  Local Time Step      1.1136e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.9673          14.206          1.6307         0.39323
v  Velocity[Y]             -11.076          16.238          1.3973         0.93899
v  Velocity[Z]             -18.176          10.738         -1.0647       -0.014924
v  ǁVelocityǁ             0.027504          20.977          6.3296           7.468
v  Pressure                 -28709      2.0533e+05       1.341e+05      1.0755e+05
v  k                     1.795e-07          5.2361        0.071247         0.11143
v  epsilon              0.00047768      1.2271e+06          1701.9          58.924
v  TurbVisc             2.0882e-12          0.5151       0.0035787        0.050361
v  CourantNb                0.2632      8.9798e+05          400.06          82.032
v  FourierNb               0.22758      2.3653e+06          219.05          3.4639
v  total_pressure       4.7129e+05      7.0533e+05       6.341e+05      6.0755e+05
v  Local Time Step            0.01        0.047752            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4557      3.0236e+06          619.12          85.496


 TIME FOR THE TIME STEP              781:        0.18555E+03

===============================================================


 INSTANT    0.782000000E+02   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         0.631973298E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160829E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16768E+02 0.55409E+01
   Friction velocity        uet   :  0.46418E-01 0.35487E+02
   Friction velocity        uk    :  0.47824E-01 0.35487E+02
   Dimensionless distance   yplus :  0.26742E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13565
   Nb of faces within the viscous sub-layer     :      11145
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49039E+01     638   0.24667E+00   0.13216E+02 0.47271E+01 
c  Velocity[X]                                      0.33518E+01 
c  Velocity[Y]                                      0.68685E+01 
c  Velocity[Z]                                      0.29957E+01 
c  Pressure     0.10532E+00     887   0.75104E-02   0.21574E-01 0.44288E-01 
c  k            0.57920E+00     162   0.62248E-04   0.85904E-03 0.13244E+01 
c  epsilon      0.39851E+04     104   0.58363E-03   0.10409E+07 0.14886E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.1501e-05                             5
a  epsilon                 -4.4494                             4
a  Local Time Step      1.2194e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5036          14.363          1.6257         0.39328
v  Velocity[Y]             -11.257            15.8          1.3787         0.93971
v  Velocity[Z]             -14.282          10.785         -1.0687       -0.015566
v  ǁVelocityǁ             0.028528          18.956          6.3522          7.4586
v  Pressure                 -28746      2.0543e+05      1.3415e+05      1.0757e+05
v  k                    4.9405e-07          5.4795        0.071456         0.11141
v  epsilon               0.0072493      1.3238e+06          1752.8              59
v  TurbVisc             1.8272e-12          0.5151       0.0035727        0.050358
v  CourantNb              0.044688      8.2006e+05          403.09          82.196
v  FourierNb               0.22753      2.3653e+06          219.05          3.4632
v  total_pressure       4.7125e+05      7.0543e+05      6.3415e+05      6.0757e+05
v  Local Time Step            0.01        0.052527            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6723      2.7998e+06          622.14          85.659


 TIME FOR THE TIME STEP              782:        0.18484E+03

===============================================================


 INSTANT    0.783000000E+02   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        -0.476341324E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160440E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17410E+02 0.55411E+01
   Friction velocity        uet   :  0.44569E-01 0.45559E+02
   Friction velocity        uk    :  0.44875E-01 0.45559E+02
   Dimensionless distance   yplus :  0.29692E-02 0.24880E+02
   ----------------------------------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48939E+01     636   0.24240E+00   0.10407E+02 0.41954E+01 
c  Velocity[X]                                      0.32467E+01 
c  Velocity[Y]                                      0.43302E+01 
c  Velocity[Z]                                      0.28305E+01 
c  Pressure     0.10379E+00     811   0.71390E-02   0.21266E-01 0.26379E-01 
c  k            0.57912E+00     179   0.68440E-04   0.10415E-02 0.14586E+01 
c  epsilon      0.39725E+04     110   0.72357E-03   0.14487E+07 0.17945E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0031875                            54
a  epsilon                 -102.45                           123
a  Local Time Step      1.1259e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5219          14.133          1.6578         0.39372
v  Velocity[Y]             -11.115          16.208          1.3481          0.9416
v  Velocity[Z]             -15.734          10.402         -1.0384       -0.014794
v  ǁVelocityǁ             0.011054           19.32          6.2922          7.4599
v  Pressure                 -28740      2.0538e+05      1.3408e+05      1.0756e+05
v  k                    2.4531e-07          5.4377        0.070383         0.11133
v  epsilon               0.0027903      1.2965e+06            1676          58.698
v  TurbVisc             1.5557e-12          0.5151       0.0035848         0.05035
v  CourantNb               0.33852      8.8816e+05          399.55          82.008
v  FourierNb               0.22717      2.3653e+06          219.07          3.4634
v  total_pressure       4.7126e+05      7.0538e+05      6.3408e+05      6.0756e+05
v  Local Time Step            0.01        0.063557            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6765      2.9056e+06          618.62          85.471


 TIME FOR THE TIME STEP              784:        0.17267E+03

===============================================================


 INSTANT    0.785000000E+02   TIME STEP NUMBER             785
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces         ------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48939E+01     636   0.24240E+00   0.10407E+02 0.41954E+01 
c  Velocity[X]                                      0.32467E+01 
c  Velocity[Y]                                      0.43302E+01 
c  Velocity[Z]                                      0.28305E+01 
c  Pressure     0.10379E+00     811   0.71390E-02   0.21266E-01 0.26379E-01 
c  k            0.57912E+00     179   0.68440E-04   0.10415E-02 0.14586E+01 
c  epsilon      0.39725E+04     110   0.72357E-03   0.14487E+07 0.17945E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0031875                            54
a  epsilon                 -102.45                           123
a  Local Time Step      1.1259e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5219          14.133          1.6578         0.------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48939E+01     636   0.24240E+00   0.10407E+02 0.41954E+01 
c  Velocity[X]                                      0.32467E+01 
c  Velocity[Y]                                      0.43302E+01 
c  Velocity[Z]                                      0.28305E+01 
c  Pressure     0.10379E+00     811   0.71390E-02   0.21266E-01 0.26379E-01 
c  k            0.57912E+00     179   0.68440E-04   0.10415E-02 0.14586E+01 
c  epsilon      0.39725E+04     110   0.72357E-03   0.14487E+07 0.17945E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0031875                            54
a  epsilon                 -102.45                           123
a  Local Time Step      1.1259e-08                        281785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5219          14.133          1.6578         0.39372
v  Velocity[Y]             -11.115          16.208          1.3481          0.9416
v  Velocity[Z]             -15.734          10.402         -1.0384       -0.014794
v  ǁVelocityǁ             0.011054           19.32          6.2922          7.4599
v  Pressure                 -28740      2.0538e+05      1.3408e+05      1.0756e+05
v  k                    2.4531e-07          5.4377        0.070383         0.11133
v  epsilon               0.0027903      1.2965e+06            1676          58.698
v  TurbVisc             1.5557e-12          0.5151       0.0035848         0.05035
v  CourantNb               0.33852      8.8816e+05          399.55          82.008
v  FourierNb               0.22717      2.3653e+06          219.07          3.4634
v  total_pressure       4.7126e+05      7.0538e+05      6.3408e+05      6.0756e+05
v  Local Time Step            0.01        0.063557            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6765      2.9056e+06          618.62          85.471


 TIME FOR THE TIME STEP              784:        0.18297E+03

===============================================================


 INSTANT    0.785000000E+02   TIME STEP NUMBER             7Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.223229326E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160851E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17112E+02 0.55409E+01
   Friction velocity        uet   :  0.33412E-01 0.51150E+02
   Friction velocity        uk    :  0.32911E-01 0.51150E+02
   Dimensionless distance   yplus :  0.30819E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13548
   Nb of faces within the viscous sub-layer     :      11206
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49060E+01     642   0.24762E+00   0.12649E+02 0.46236E+01 
c  Velocity[X]                                      0.35386E+01 
c  Velocity[Y]                                      0.60364E+01 
c  Velocity[Z]                                      0.30743E+01 
c  Pressure     0.10217E+00     976   0.71490E-02   0.20923E-01 0.51354E-01 
c  k            0.57913E+00     174   0.68419E-04   0.98862E-03 0.14211E+01 
c  epsilon      0.39695E+04     100   0.69232E-03   0.10964E+07 0.15375E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00085139                             7
a  epsilon                   -38.1                            18
a  Local Time Step      1.2058e-08                        281788


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5077          14.135          1.6269         0.39319
v  Velocity[Y]             -11.163          15.718          1.3684         0.93955
v  Velocity[Z]               -16.1          10.494         -1.0689      Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.223229326E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160851E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17112E+02 0.55409E+01
   Friction velocity        uet   :  0.33412E-01 0.51150E+02
   Friction velocity        uk    :  0.32911E-01 0.51150E+02
   Dimensionless distance   yplus :  0.30819E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13548
   Nb of faces within the viscous sub-layer     :      11206
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
--------------------------------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.223229326E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160851E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17112E+02 0.55409E+01
   Friction velocity        uet   :  0.33412E-01 0.51150E+02
   Friction velocity        uk    :  0.32911E-01 0.51150E+02
   Dimensionless distance   yplus :  0.30819E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13548
   Nb of faces within the viscous sub-layer     :      11206
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49060E+01     642   0.24762E+00   0.12649E+02 0.46236E+01 
c  Velocity[X]                                      0.35386E+01 
c  Velocity[Y]                                      0.60364E+01 
c  Velocity[Z]                                      0.30743E+01 
c  Pressure     0.10217E+00     976   0.71490E-02   0.20923E-01 0.51354E-01 
c  k            0.57913E+00     174   0.68419E-04   0.98862E-03 0.14211E+01 
c  epsilon      0.39695E+04     100   0.69232E-03   0.10964E+07 0.15375E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00085139                             7
a  epsilon                   -38.1                            18
a  Local Time Step      1.2058e-08                        281788


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  ---v  Velocity[Z]             -15.669          9.7493          -1.062       -0.015656
v  ǁVelocityǁ             0.011164          19.141          6.2816          7.4605
v  Pressure                 -28693      2.0549e+05      1.3418e+05      1.0763e+05
v  k                    5.5482e-07          5.5648        0.072153         0.11137
v  epsilon               0.0056434      1.3548e+06          1808.4           59.16
v  TurbVisc             1.6577e-12          0.5151       0.0035748        0.050342
v  CourantNb               0.11414      9.0538e+05          408.14          82.161
v  FourierNb                0.2267      2.3653e+06          219.04          3.4629
v  total_pressure       4.7131e+05      7.0549e+05      6.3418e+05      6.0763e+05
v  Local Time Step            0.01        0.084595            0.01        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6213      2.7948e+06          627.18          85.624


 TIME FOR THE TIME STEP              787:        0.18717E+03

===============================================================


 INSTANT    0.788000000E+02   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         0.100556894E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160433E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17170E+02 0.55410E+01
   Friction velocity        uet   :  0.38797E-01 0.41853E+02
   Friction velocity        uk    :  0.38252E-01 0.41853E+02
   Dimensionless distance   yplus :  0.19016E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13509
   Nb of faces within the viscous sub-layer     :      11190
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-------------v  Velocity[Z]             -15.669          9.7493          -1.062       -0.015656
v  ǁVelocityǁ             0.011164          19.141          6.2816          7.4605
v  Pressure                 -28693      2.0549e+05      1.3418e+05      1.0763e+05
v  k                    5.5482e-07          5.5648        0.072153         0.11137
v  epsilon               0.0056434      1.3548e+06          1808.4           59.16
v  TurbVisc             1.6577e-12          0.5151       0.0035748        0.050342
v  CourantNb               0.11414      9.0538e+05          408.14          82.161
v  FourierNb                0.2267      2.3653e+06          219.04          3.4629
v  total_pressure       4.7131e+05      7.0549e+05      6.3418e+05      6.0763e+05
v  Local Time Step            0.01        0.084595            0.01        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6213      2.7948e+06          627.18          85.624


 TIME FOR THE TIME STEP              787:        0.18845E+03

===============================================================


 INSTANT    0.788000000E+02   TIME STEP NUMBER             788
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet         v  Velocity[Z]             -15.669          9.7493          -1.062       -0.015656
v  ǁVelocityǁ             0.011164          19.141          6.2816          7.4605
v  Pressure                 -28693      2.0549e+05      1.3418e+05      1.0763e+05
v  k                    5.5482e-07          5.5648        0.072153         0.11137
v  epsilon               0.0056434      1.3548e+06          1808.4           59.16
v  TurbVisc             1.6577e-12          0.5151       0.0035748        0.050342
v  CourantNb               0.11414      9.0538e+05          408.14          82.161
v  FourierNb                0.2267      2.3653e+06          219.04          3.4629
v  total_pressure       4.7131e+05      7.0549e+05      6.3418e+05      6.0763e+05
v  Local Time Step            0.01        0.084595            0.01        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6213      2.7948e+06          627.18          85.624


 TIME FOR THE TIME STEP              787:        0.18861E+03

===============================================================


 INSTANT    0.788000000E+02   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         0.100556894E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160433E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17170E+02 0.55410E+01
   Friction velocity        uet   :  0.38797E-01 0.41853E+02
   Friction velocity        uk    :  0.38252E-01 0.41853E+02
   Dimensionless distance   yplus :  0.19016E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13509
   Nb of faces within the viscous sub-layer     :      11190
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48961E+01     616   0.24226E+00   0.12409E+02 0.45811E+01 
c  Velocity[X]                                      0.39264E+01 
c  Velocity[Y]                                      0.55848E+01 
c  Velocity[Z]                                      0.28976E+01 
c  Pressure     0.10558E+00     832   0.72756E-02   0.21637E-01 0.26822E-01 
c  k            0.57919E+00     168   0.74358E-04   0.11127E-02 0.15074E+01 
c  epsilon      0.40037E+04     110   0.70751E-03   0.17845E+07 0.19706E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0067735                            58
a  epsilon                 -197.23                           125
a  Local Time Step      1.1366e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6784          14.119          1.6693         0.39334
v  Velocity[Y]             -10.951          16.229          1.3427         0.94063
v  Velocity[Z]             -18.306          11.258         -1.0285       -0.015206
v  ǁVelocityǁ            0.0035174          21.022          6.2805          7.4615
v  Pressure                 -28653      2.0543e+05      1.3415e+05      1.0762e+05
v  k                    2.2346e-07          5.5044        0.070681         0.11138
v  epsilon              0.00093638      1.3248e+06          1693.4          58.767
v  TurbVisc             1.6209e-12          0.5151       0.0035952        0.050347
v  CourantNb               0.11802       8.798e+05          400.82          81.989
v  FourierNb                0.2268      2.3653e+06          219.07          3.4645
v  total_pressure       4.7135e+05      7.0543e+05      6.3415e+05      6.0762e+05
v  Local Time Step            0.01        0.045527            0.01        0.010003


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6146       2.952e+06           619.9          85.453


 TIME FOR THE TIME STEP              788:        0.17921E+03

===============================================================


 INSTANT    0.789000000E+02   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         0.336245020E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160834E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16917E+02 0.55410E+01
   Friction velocity        uet   :  0.41996E-01 0.50916E+02
   Friction velocity        uk    :  0.45163E-01 0.50916E+02
   Dimensionless distance   yplus :  0.36937E-02 0.24879E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13536
   Nb of faces within the viscous sub-layer     :      11216
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48951E+01     650   0.24190E+00   0.13136E+02 0.47105E+01 
c  Velocity[X]                                      0.29886E+01 
c  Velocity[Y]                                      0.71305E+01 
c  Velocity[Z]                                      0.30168E+01 
c  Pressure     0.10397E+00     991   0.76405E-02   0.21302E-01 0.65491E-01 
c  k            0.57916E+00     151   0.76402E-04   0.11043E-02 0.15017E+01 
c  epsilon      0.39057E+04     103   0.53545E-03   0.12910E+07 0.17216E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0013118                             8
a  epsilon                 -208.25                            34
a  Local Time Step        1.19e-08                        281781


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7687          13.975          1.6305         0.39396
v  Velocity[Y]             -11.087          15.646          1.3562          0.9401
v  Velocity[Z]             -15.635          10.633         -1.0688       -0.014664
v  ǁVelocityǁ            0.0093479          18.812          6.3143          7.4636
v  Pressure                 -28687      2.0535e+05      1.3406e+05      1.0755e+05
v  k                    4.6401e-07          5.3215        0.070191         0.11141
v  epsilon              0.00036791      1.2559e+06          1638.5          58.783
v  TurbVisc             2.2142e-12          0.5151         0.00358        0.050352
v  CourantNb              0.099918      8.4035e+05          397.69           82.11
v  FourierNb               0.22698      2.3653e+06          219.05          3.4637
v  total_pressure       4.7131e+05      7.0535e+05      6.3406e+05      6.0755e+05
v  Local Time Step            0.01         0.05008            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6327       2.943e+06          616.73          85.574


 TIME FOR THE TIME STEP              789:        0.17874E+03

===============================================================


 INSTANT    0.790000000E+02   TIME STEP NUMBER             790
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
----------------------------------------------Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160432E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17042E+02 0.55410E+01
   Friction velocity        uet   :  0.40949E-01 0.36430E+02
   Friction velocity        uk    :  0.39362E-01 0.36430E+02
   Dimensionless distance   yplus :  0.15856E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13564
   Nb of faces within the viscous sub-layer     :      11135
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48982E+01     643   0.23756E+00   0.13613E+02 0.47955E+01 
c  Velocity[X]                                      0.32865E+01 
c  Velocity[Y]                                      0.77126E+01 
c  Velocity[Z]                                      0.26139E+01 
c  Pressure     0.10503E+00     937   0.76838E-02   0.21501E-01 0.55086E-01 
c  k            0.57923E+00     163   0.90114E-04   0.12974E-02 0.16275E+01 
c  epsilon      0.40813E+04     102   0.10701E-02   0.35052E+07 0.26409E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00067526                            13
a  epsilon                 -21.199                            11
a  Local Time Step      1.0858e-08                        281778


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.8568          14.275          1.6426         0.39285
v  Velocity[Y]             -11.113           16.22          1.3657          0.9403
v  Velocity[Z]              -15.31          12.193          -1.063       -0.015743
v  ǁVelocityǁ             0.018988          19.103          6.2942          7.4597
v  Pressure                 -28721      2.0545e+05      1.3415e+05      1.0762e+05
v  k                    5.7601e-07          5.4751        0.072165         0.11143
v  epsilon               0.0072979      1.3255e+06    Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160432E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17042E+02 0.55410E+01
   Friction velocity        uet   :  0.40949E-01 0.36430E+02
   Friction velocity        uk    :  0.39362E-01 0.36430E+02
   Dimensionless distance   yplus :  0.15856E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13564
   Nb of faces within the viscous sub-layer     :      11135
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48982E+01     643   0.23756E+00   0.13613E+02 0.47955E+01 
c  Velocity[X]                       Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160432E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17042E+02 0.55410E+01
   Friction velocity        uet   :  0.40949E-01 0.36430E+02
   Friction velocity        uk    :  0.39362E-01 0.36430E+02
   Dimensionless distance   yplus :  0.15856E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13564
   Nb of faces within the viscous sub-layer     :      11135
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48982E+01     643   0.23756E+00   0.13613E+02 0.47955E+01 
c  Velocity[X]                                      0.32865E+01 
c  Velocity[Y]                                      0.77126E+01 
c  Velocity[Z]                                      0.26139E+01 
c  Pressure     0.10503E+00     937   0.76838E-02   0.21501E-01 0.55086E-01 
c  k            0.57923E+00     163   0.90114E-04   0.12974E-02 0.16275E+01 
c  epsilon      0.40813E+04     102   0.10701E-02   0.35052E+07 0.26409E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00067526                            13
a  epsilon                 -21.199                            11
a  Local Time Step      1.0858e-08                        281778


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.8568          14.275          1.6426         0.39285
v  Velocity[Y]             -11.113           16.22          1.3657          0.9403
v  Velocity[Z]              -15.31          12.193          -1.063       -0.015743
v  ǁVelocityǁ             0.018988     v  epsilon               0.0003467      1.3773e+06          1729.7          58.818
v  TurbVisc             1.7802e-12          0.5151       0.0035927        0.050354
v  CourantNb               0.19959      9.2019e+05          402.58          81.989
v  FourierNb               0.22703      2.3653e+06          219.08          3.4651
v  total_pressure       4.7122e+05      7.0537e+05      6.3406e+05      6.0755e+05
v  Local Time Step            0.01        0.063666        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6763      3.0458e+06          621.65          85.454


 TIME FOR THE TIME STEP              792:        0.18421E+03

===============================================================


 INSTANT    0.793000000E+02   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         0.953558732E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160840E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17048E+02 0.55411E+01
   Friction velocity        uet   :  0.42198E-01 0.45074E+02
   Friction velocity        uk    :  0.48497E-01 0.45074E+02
   Dimensionless distance   yplus :  0.30704E-02 0.24879E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13567
   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     0.48954E+01     629   0.24153E+00   0.11374E+02 0.43842E+01 
c  Velocity[X]                                      0.29603E+01 
c  Velocity[Y]                                      0.56676E+01 
c  Velocity[Z]                                      0.27465E+0v  epsilon               0.0003467      1.3773e+06          1729.7          58.818
v  TurbVisc             1.7802e-12          0.5151       0.0035927        0.050354
v  CourantNb               0.19959      9.2019e+05          402.58          81.989
v  FourierNb               0.22703      2.3653e+06          219.08          3.4651
v  total_pressure       4.7122e+05      7.0537e+05      6.3406e+05      6.0755e+05
v  Local Time Step            0.01        0.063666        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6763      3.0458e+06          621.65          85.454


 TIME FOR THE TIME STEP              792:        0.18462E+03

===============================================================


 INSTANT    0.793000000E+02   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         0.953558732E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160840E+01
Free inlet               13 v  epsilon               0.0003467      1.3773e+06          1729.7          58.818
v  TurbVisc             1.7802e-12          0.5151       0.0035927        0.050354
v  CourantNb               0.19959      9.2019e+05          402.58          81.989
v  FourierNb               0.22703      2.3653e+06          219.08          3.4651
v  total_pressure       4.7122e+05      7.0537e+05      6.3406e+05      6.0755e+05
v  Local Time Step            0.01        0.063666        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6763      3.0458e+06          621.65          85.454


 TIME FOR THE TIME STEP              792:        0.18954E+03

===============================================================


 INSTANT    0.793000000E+02   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         0.953558732E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160840E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17048E+02 0.55411E+01
   Friction velocity        uet   :  0.42198E-01 0.45074E+02
   Friction velocity        uk    :  0.48497E-01 0.45074E+02
   Dimensionless distance   yplus :  0.30704E-02 0.24879E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13567
   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     0.48954E+01     629   0.24153E+00   0.11374E+02 0.43842E+01 
c  Velocity[X]                                      0.29603E+01 
c  Velocity[Y]                                      0.56676E+01 
c  Velocity[Z]                                      0.27465E+01 
c  Pressure     0.10597E+00     869   0.76805E-02   0.21717E-01 0.37557E-01 
c  k            0.57916E+00     159   0.70903E-04   0.10423E-02 0.14588E+01 
c  epsilon      0.38986E+04     102   0.71102E-03   0.18643E+07 0.20806E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0062675                            27
a  epsilon                 -731.09                            70
a  Local Time Step      1.1816e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4601          14.075          1.6378         0.39343
v  Velocity[Y]             -11.291          15.837          1.3098         0.94244
v  Velocity[Z]             -17.034          11.733         -1.0462       -0.014389
v  ǁVelocityǁ             0.016447          19.811          6.2953          7.4618
v  Pressure                 -28806      2.0534e+05      1.3402e+05      1.0752e+05
v  k                    3.7796e-09          5.2104        0.069933         0.11142
v  epsilon              0.00034534      1.2192e+06          1626.2          58.661
v  TurbVisc             2.0893e-12          0.5151        0.003581        0.050354
v  CourantNb             0.0065629      8.4629e+05           396.5          82.072
v  FourierNb               0.22696      2.3653e+06          219.05          3.4645
v  total_pressure       4.7119e+05      7.0534e+05      6.3402e+05      6.0752e+05
v  Local Time Step            0.01        0.070032        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5907      2.8982e+06          615.56          85.536


 TIME FOR THE TIME STEP              793:        0.17655E+03

===============================================================


 INSTANT    0.794000000E+02   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         0.277010710E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160841E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17135E+02 0.55410E+01
   Friction velocity        uet   :  0.17404E-01 0.63277E+02
   Friction velocity        uk    :  0.25699E-01 0.63277E+02
   Dimensionless distance   yplus :  0.94176E-03 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13589
   Nb of faces within the viscous sub-layer     :      11204
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48982E+01     641   0.24189E+00   0.13917E+02 0.48459E+01 
c  Velocity[X]                                      0.36365E+01 
c  Velocity[Y]                                      0.81472E+01 
c  Velocity[Z]                                      0.21335E+01 
c  Pressure     0.10705E+00     383   0.74724E-02   0.21915E-01 0.20131E-01 
c  k            0.57922E+00     170   0.82593E-04   0.12148E-02 0.15749E+01 
c  epsilon      0.39493E+04     105   0.98826E-03   0.21301E+07 0.21277E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0016643                            16
a  epsilon                  -55.91                            25
a  Local Time Step      1.1488e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6407          14.116          1.6272          0.3928
v  Velocity[Y]             -11.428          15.879          1.4009         0.93972
v  Velocity[Z]             -16.042          12.457         -1.0759       -0.014295
v  ǁVelocityǁ              0.01094          18.806          6.3492          7.4667
v  Pressure                 -28814      2.0532e+05      1.3402e+05      1.0752e+05
v  k                    4.3603e-07          5.4067        0.072054         0.11144
v  epsilon                 0.00127      1.2839e+06            1756          59.155
v  TurbVisc             3.5624e-14          0.5151       0.0035877        0.050354
v  CourantNb               0.03724      8.7049e+05          399.82          82.075
v  FourierNb               0.22711      2.3653e+06          219.04          3.4643
v  total_pressure       4.7119e+05      7.0532e+05      6.3402e+05      6.0752e+05
v  Local Time Step            0.01        0.076633        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5946      2.6771e+06          618.86          85.539


 TIME FOR THE TIME STEP              794:        0.16140E+03

===============================================================


 INSTANT    0.795000000E+02   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        -0.872871554E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0       Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17260E+02 0.55409E+01
   Friction velocity        uet   :  0.23973E-01 0.59661E+02
   Friction velocity        uk    :  0.38138E-01 0.59661E+02
   Dimensionless distance   yplus :  0.31423E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13487
   Nb of faces within the viscous sub-layer     :      11149
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48996E+01     658   0.24578E+00   0.11934E+02 0.44895E+01 
c  Velocity[X]                                      0.33308E+01 
c  Velocity[Y]                                      0.63442E+01 
c  Velocity[Z]                                      0.22588E+01 
c  Pressure     0.10565E+00     946   0.74098E-02   0.21659E-01 0.55243E-01 
c  k            0.57926E+00     176   0.76428E-04   0.12566E-02 0.16018E+01 
c  epsilon      0.40483E+04      96   0.74567E-03   0.21575E+07 0.21269E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0043258                            30
a  epsilon                 -152.76                            78
a  Local Time Step      1.0699e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.663          14.201            1.66         0.39214
v  Velocity[Y]             -11.019          15.892          1.3361         0.94224
v  Velocity[Z]             -15.899          11.805         -1.0346       -0.015496
v  ǁVelocityǁ             0.018901          18.939           6.274          7.4631
v  Pressure                 -28865      2.0529e+05      1.3398e+05      1.0746e+05
v  k                    1.3402e-07          6.0272        0.071237         0.11143
v  epsilon              0.00027465      1.3868e+06          1740.8          58.852
v  TurbVisc             1.8002e-12          0.5151       0.0035881        0.050358
v  CourantNb              0.020246      9.3468e+05           403.5          82.014
v  FourierNb               0.22729      2.3653e+06          2Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17260E+02 0.55409E+01
   Friction velocity        uet   :  0.23973E-01 0.59661E+02
   Friction velocity        uk    :  0.38138E-01 0.59661E+02
   Dimensionless distance   yplus :  0.31423E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13487
   Nb of faces within the viscous sub-layer     :      11149
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48996E+01     658   0.24578E+00   0.11934E+02 0.44895E+01 
c  Velocity[X]                                      0.33308E+01 
c  Velocity[Y]                                      0.63442E+01 
c  Velocity[Z]                                      0.22588E+01 
c  Pressure     0.10565E+00     946   0.74098E-02   0.21659E-01 0.55243E-01 
c  k            0.579Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17260E+02 0.55409E+01
   Friction velocity        uet   :  0.23973E-01 0.59661E+02
   Friction velocity        uk    :  0.38138E-01 0.59661E+02
   Dimensionless distance   yplus :  0.31423E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13487
   Nb of faces within the viscous sub-layer     :      11149
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48996E+01     658   0.24578E+00   0.11934E+02 0.44895E+01 
c  Velocity[X]                                      0.33308E+01 
c  Velocity[Y]                                      0.63442E+01 
c  Velocity[Z]                                      0.22588E+01 
c  Pressure     0.10565E+00     946   0.74098E-02   0.21659E-01 0.55243E-01 
c  k            0.57926E+00     176   0.76428E-04   0.12566E-02 0.16018E+01 
c  epsilon      0.40483E+04      96   0.74567E-03   0.21575E+07 0.21269E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0043258                            30
a  epsilon                 -152.76                            78
a  Local Time Step      1.0699e-08                        281783


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.663          14.201            1.66         0.39214
v  Velocity[Y]             -11.019          15.892          1.3361         0.94224
v  Velocity[Z]             -15.899          11.805         -1.0346       -0.015496
v  ǁVelocityǁ             0.018901          18.939           6.274          7.4631
v  Pressure                 -28865      2.0529e+05      1.3398e+05      1.0746e+05
v  k                    1.3402e-07          6.0272        0.071237         0.11143
v  epsilon              0.00027465      1.3868e+06          1740.8          58.852
v  TurbVisc             1.8002e-12          0.5151       0.0035881        0.050358
v  CourantNb              0.020246      9.3468e+05           403.5          82.014
v  FourierNb               0.22729      2.3653e+06          219.07          3.4632
v  total_pressure       4.7114e+05      7.0529e+05      6.3398e+05      6.0746e+05
v  Local Time Step            0.01        0.092725        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6747      3.0603e+06          622.57          85.477


 TIME FOR THE TIME STEP              796:        0.19176E+03

===============================================================


 INSTANT    0.797000000E+02   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         0.525463566E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160850E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17117E+02 0.55410E+01
   Friction velocity        uet   :  0.42611E-01 0.43030E+02
   Friction velocity        uk    :  0.45697E-01 0.43030E+02
   Dimensionless distance   yplus :  0.44144E-02 0.24879E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13569
   Nb of faces within the viscous sub-layer     :      11186
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48952E+01     655   0.24590E+00   0.97562E+01 0.40617E+01 
c  Velocity[X]                                      0.28287E+01 
c  Velocity[Y]                                      0.44557E+01 
c  Velocity[Z]                                      0.24718E+01 
c  Pressure     0.98316E-01     852   0.68638E-02   0.20144E-01 0.25652E-01 
c  k            0.57923E+00     171   0.77074E-04   0.11651E-02 0.15424E+01 
c  epsilon      0.39629E+04     102   0.73050E-03   0.15436E+07 0.18489E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0005705                            11
a  epsilon                 -51.354                            25
a  Local Time Step      1.1959e-08                        281781


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5723          14.047          1.6462         0.39366
v  Velocity[Y]             -11.355          16.177          1.3339         0.94184
v  Velocity[Z]             -19.102          11.366         -1.0545       -0.014884
v  ǁVelocityǁ             0.011051          21.794          6.3078          7.4605
v  Pressure                 -28807      2.0532e+05        1.34e+05      1.0749e+05
v  k                    2.0138e-07          5.2335        0.070772         0.11143
v  epsilon               0.0008258      1.2285e+06          1687.8          58.942
v  TurbVisc             2.0554e-12          0.5151       0.0035873         0.05036
v  CourantNb              0.067968      8.3617e+05          398.36          82.044
v  FourierNb               0.22736      2.3653e+06          219.07          3.4635
v  total_pressure       4.7119e+05      7.0532e+05        6.34e+05      6.0749e+05
v  Local Time Step            0.01           0.102        0.010001        0.010006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6041      2.8607e+06          617.43          85.508


 TIME FOR THE TIME STEP              797:        0.17954E+03

===============================================================


 INSTANT    0.798000000E+02   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         0.105623727E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160418E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16949E+02 0.55410E+01
   Friction velocity        uet   :  0.45972E-01 0.62844E+02
   Friction velocity        uk    :  0.47275E-01 0.62844E+02
   Dimensionless distance   yplus :  0.41668E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13547
   Nb of faces within the viscous sub-layer     :      11141
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48968E+01     630   0.24705E+00   0.12583E+02 0.46098E+01 
c  Velocity[X]                                      0.30852E+01 
c  Velocity[Y]                                      0.73717E+01 
c  Velocity[Z]                                      0.21263E+01 
c  Pr@      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     0.48952E+01     620   0.24383E+00   0.10905E+02 0.42940E+01 
c  Velocity[X]                                      0.32341E+01 
c  Velocity[Y]                                      0.49907E+01 
c  Velocity[Z]                                      0.26799E+01 
c  Pressure     0.10442E+00     667   0.72153E-02   0.21396E-01 0.24837E-01 
c  k            0.57925E+00     172   0.87698E-04   0.12156E-02 0.15754E+01 
c  epsilon      0.40488E+04     103   0.80621E-03   0.21717E+07 0.21110E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00046062                            27
a  epsilon                 -23.819                            32
a  Local Time Step      1.0743e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6955          14.198          1.6388         0.39272
v  Velocity[Y]             -11.077          16.293          1.3736         0.93989
v  Velocity[Z]             -18.347          10.908         -1.0526       -0.015667
v  ǁVelocityǁ            0.0041968          21.094          6.3083          7.4577
v  Pressure                 -28816      2.0529e+05      1.3398e+05      1.0745e+05
v  k                    4.9412e-07          5.3989        0.072253         0.11141
v  epsilon               0.0015916      1.2938e+06          1791.2          59.238
v  TurbVisc             7.2463e-13          0.5151       0.0035756        0.050353
v  CourantNb               0.21277      9.3083e+05          406.26          82.153
v  FourierNb               0.22738      2.3653e+06          219.07          3.4646
v  total_pressure       4.7118e+05      7.0529e+05      6.3398e+05      6.0745e+05
v  Local Time Step            0.01         0.10052        0.010001        0.010005


  ** Computed values on cells
   @      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     0.48952E+01     620   0.24383E+00   0.10905E+02 0.42940E+01 
c  Velocity[X]                                      0.32341E+01 
c  Velocity[Y]                                      0.49907E+01 
c  Velocity[Z]                                      0.26799E+01 
c  Pressure     0.10442E+00     667   0.72153E-02   0.21396E-01 0.24837E-01 
c  k            0.57925E+00     172   0.87698E-04   0.12156E-02 0.15754E+01 
c  epsilon      0.40488E+04     103   0.80621E-03   0.21717E+07 0.21110E+02 
-----------------------------------------------------------------------------
  
  

  ** @      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     0.48952E+01     620   0.24383E+00   0.10905E+02 0.42940E+01 
c  Velocity[X]                                      0.32341E+01 
c  Velocity[Y]                                      0.49907E+01 
c  Velocity[Z]                                      0.26799E+01 
c  Pressure     0.10442E+00     667   0.72153E-02   0.21396E-01 0.24837E-01 
c  k            0.57925E+00     172   0.87698E-04   0.12156E-02 0.15754E+01 
c  epsilon      0.40488E+04     103   0.80621E-03   0.21717E+07 0.21110E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00046062                            27
a  epsilon                 -23.819                            32
a  Local Time Step      1.0743e-08                        281782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6955          14.198          1.6388         0.39272
v  Velocity[Y]             -11.077          16.293          1.3736         0.93989
v  Velocity[Z]             -18.347          10.908         -1.0526       -0.015667
v  ǁVelocityǁ            0.0041968          21.094          6.3083          7.4577
v  Pressure                 -28816      2.0529e+05      1.3398e+05      1.0745e+05
v  k                    4.9412e-07          5.3989        0.072253         0.11141
v  epsilon               0.0015916      1.2938e+06          1791.2          59.238
v  TurbVisc             7.2463e-13          0.5151       0.0035756        0.050353
v  CourantNb               0.21277      9.3083e+05          406.26          82.153
v  FourierNb               0.22738      2.3653e+06          219.07          3.4646
v  total_pressure       4.7118e+05      7.0529e+05      6.3398e+05      6.0745e+05
v  Local Time Step            0.01         0.10052        0.010001        0.010005


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6868      2.8029e+06          625.33          85.618


 TIME FOR THE TIME STEP              799:        0.46175E+02

===============================================================


 INSTANT    0.800000000E+02   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        -0.525404789E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160806E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16936E+02 0.55409E+01
   Friction velocity        uet   :  0.45456E-01 0.60712E+02
   Friction velocity        uk    :  0.50497E-01 0.60712E+02
   Dimensionless distance   yplus :  0.24513E-02 0.24880E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13502
   Nb of faces within the viscous sub-layer     :      11140
   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+02


   ** 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 the external forces                      
 End writing


 Time for restart files:    0.47338E-01



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48960E+01     677   0.24449E+00   0.11722E+02 0.44490E+01 
c  Velocity[X]                                      0.34949E+01 
c  Velocity[Y]                                      0.62052E+01 
c  Velocity[Z]                                      0.20221E+01 
c  Pressure     0.10393E+00     923   0.71258E-02   0.21309E-01 0.36618E-01 
c  k            0.57920E+00     166   0.63065E-04   0.10426E-02 0.14592E+01 
c  epsilon      0.40733E+04      95   0.45178E-03   0.12329E+07 0.16047E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0022787                            24
a  epsilon                 -163.41                            52
a  Local Time Step       1.079e-08                        281784


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6077          14.183          1.6549         0.39262
v  Velocity[Y]             -11.186          15.885          1.3384         0.94146
v  Velocity[Z]             -15.019          10.849         -1.0318       -0.015318
v  ǁVelocityǁ             0.019645          18.856          6.2779          7.4644
v  Pressure                 -28841      2.0524e+05      1.3392e+05      1.0742e+05
v  k                    2.3039e-08           5.608        0.071142         0.11138
v  epsilon              0.00020592        1.36e+06          1740.5          58.789
v  TurbVisc             2.0258e-12          0.5151       0.0035843        0.050355
v  CourantNb              0.054346      9.2683e+05          404.22          82.006
v  FourierNb               0.22733      2.3653e+06          219.09           3.465
v  total_pressure       4.7116e+05      7.0524e+05      6.3392e+05      6.0742e+05
v  Local Time Step            0.01        0.072293            0.01        0.010004


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6748      3.0525e+06          623.31          85.471


 TIME FOR THE TIME STEP              800:        0.38134E+02

===============================================================



===============================================================



                 FINAL STAGE OF THE CALCULATION              
                 ==============================              


 =========================================================== 




   ** TIME FOR FINAL WRITING:    0.17389E-03
      -----------------------                                



 =========================================================== 




                      END OF CALCULATION                     
                      ==================                     


===============================================================

 Destroying structures and ending computation

e+06          623.31          85.471


 TIME FOR THE TIME STEP              800:        0.17415E+03

===============================================================



===============================================================



                 FINAL STAGE OF THE CALCULATION              
                 ==============================              


 =========================================================== 




   ** TIME FOR FINAL WRITING:    0.29300E-03
      -----------------------                                



 =========================================================== 




                      END OF CALCULATION                     
                      ==================                     


===============================================================

 Destroying structures and ending computation


Calculation time summary:

  User CPU time:         129966.695 s
  System CPU time:          296.048 s

  Elapsed time:          138141.189 s
  CPU / elapsed time          0.943

Memory use summary:

  Total memory used:                             702.820 MiB
  Theoretical instrumented dynamic memory:       346.407 MiB

Calculation time summary:

  User CPU time:         130234.477 s
  System CPU time:          261.288 s

  Elapsed time:          138176.560 s
  CPU / elapsed time          0.944

Memory use summary:

  Total memory used:                             702.820 MiB
  Theoretical instrumented dynamic memory:       346.407 MiB

Calculation time summary:

  User CPU time:         129976.398 s
  System CPU time:          291.164 s

  Elapsed time:          138182.203 s
  CPU / elapsed time          0.943

Memory use summary:

  Total memory used:                             702.820 MiB
  Theoretical instrumented dynamic memory:       346.407 MiB

Calculation time summary:

  User CPU time:         129938.102 s
  System CPU time:          296.272 s

  Elapsed time:          138192.054 s
  CPU / elapsed time          0.942

Memory use summary:

  Total memory used:                             702.824 MiB
  Theoretical instrumented dynamic memory:       346.407 MiB

Calculation time summary:

  User CPU time:         130067.703 s
  System CPU time:          300.504 s

  Elapsed time:          138213.535 s
  CPU / elapsed time          0.943

Memory use summary:

  Total memory used:                             702.820 MiB
  Theoretical instrumented dynamic memory:       346.407 MiB

Calculation time summary:

  User CPU time:         129850.188 s
  System CPU time:          290.360 s

  Elapsed time:          138261.276 s
  CPU / elapsed time          0.941

Memory use summary:

  Total memory used:                             702.820 MiB
  Theoretical instrumented dynamic memory:       346.407 MiB
